메뉴 건너뛰기




Volumn 40, Issue 6, 2003, Pages 1047-1065

Aeroelasticity of nonconventional airplane configurations - Past and future

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; AEROSPACE ENGINEERING; HISTORY; SENSORS; WINGS;

EID: 0348129533     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.7217     Document Type: Article
Times cited : (143)

References (207)
  • 1
    • 0003911590 scopus 로고
    • TYC Publishing Co., Bellevue, WA
    • Cook, W. H., The Road to the 707, TYC Publishing Co., Bellevue, WA, 1991.
    • (1991) The Road to the 707
    • Cook, W.H.1
  • 3
    • 84888707375 scopus 로고
    • What drives unique configurations
    • Society of Automotive Engineers, Inc., Warrendale, PA
    • Roskam, J., "What Drives Unique Configurations," Advanced Aerospace Aerodynamics, Society of Automotive Engineers, Inc., Warrendale, PA, 1988.
    • (1988) Advanced Aerospace Aerodynamics
    • Roskam, J.1
  • 4
    • 85039564661 scopus 로고    scopus 로고
    • A very large aircraft, a challenging project for aeroelastics and loads
    • Associacion de Ingenieros Aeronauticos de Espana, Madrid, Spain
    • Grouas, J., "A Very Large Aircraft, a Challenging Project for Aeroelastics and Loads," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2001, Vol. 1, Associacion de Ingenieros Aeronauticos de Espana, Madrid, Spain, 2001, pp. 77-88.
    • (2001) Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2001 , vol.1 , pp. 77-88
    • Grouas, J.1
  • 6
    • 0000283402 scopus 로고
    • The expanding domain of aeroelasticity
    • Aug.
    • Collar, A. R., "The Expanding Domain of Aeroelasticity," Journal of the Royal Aeronautical Society, Vol. 50, Aug. 1946, pp. 613-636.
    • (1946) Journal of the Royal Aeronautical Society , vol.50 , pp. 613-636
    • Collar, A.R.1
  • 7
    • 85003412446 scopus 로고
    • On vibration and flutter analysis with free-free boundary conditions
    • Jan.
    • Rodden, W. P., "On Vibration and Flutter Analysis with Free-free Boundary Conditions," Journal of the Aerospace Sciences, Jan. 1961, p. 66.
    • (1961) Journal of the Aerospace Sciences , pp. 66
    • Rodden, W.P.1
  • 8
    • 0016996419 scopus 로고
    • Aeroelasticity - Frontiers and beyond
    • Garrick, I. E., "Aeroelasticity - Frontiers and Beyond," Journal of Aircraft, Vol. 13, No. 9, 1976, pp. 641-657.
    • (1976) Journal of Aircraft , vol.13 , Issue.9 , pp. 641-657
    • Garrick, I.E.1
  • 9
    • 0016126294 scopus 로고
    • Static aeroelasticity and the flying wing, revisited
    • Weisshaar, T. A., and Ashley, H., "Static Aeroelasticity and the Flying Wing, Revisited," Journal of Aircraft, Vol. 11, No. 11, 1974, pp. 718-720.
    • (1974) Journal of Aircraft , vol.11 , Issue.11 , pp. 718-720
    • Weisshaar, T.A.1    Ashley, H.2
  • 10
    • 0017996943 scopus 로고
    • Aeroelastic stability characteristics of an oblique winged aircraft
    • Crittenden, J. B., Weisshaar, T. A., Johnson, E. H., and Rutkowski, M. J., "Aeroelastic Stability Characteristics of an Oblique Winged Aircraft," Journal of Aircraft, Vol. 15, No. 7, 1978, pp. 429-434.
    • (1978) Journal of Aircraft , vol.15 , Issue.7 , pp. 429-434
    • Crittenden, J.B.1    Weisshaar, T.A.2    Johnson, E.H.3    Rutkowski, M.J.4
  • 11
    • 0015488913 scopus 로고
    • New design goals and a new shape for the SST
    • Dec.
    • Jones, R. T., "New Design Goals and a New Shape for the SST," Astronautics and Aeronautics, Vol. 10, Dec. 1972, pp. 66-70.
    • (1972) Astronautics and Aeronautics , vol.10 , pp. 66-70
    • Jones, R.T.1
  • 12
    • 0022079907 scopus 로고
    • Oblique wing ready for research aircraft
    • Gregory, T. A., "Oblique Wing Ready for Research Aircraft," Aerospace America, Vol. 23, No. 6, 1985, pp. 78-83.
    • (1985) Aerospace America , vol.23 , Issue.6 , pp. 78-83
    • Gregory, T.A.1
  • 13
    • 0028282179 scopus 로고
    • Integrated structure/control concepts for oblique wing roll control and trim
    • Weisshaar, T. A., "Integrated Structure/Control Concepts for Oblique Wing Roll Control and Trim," Journal of Aircraft, No. 1, 1994.
    • (1994) Journal of Aircraft , Issue.1
    • Weisshaar, T.A.1
  • 14
    • 0025445066 scopus 로고
    • Static aeroelastic tailoring for oblique wing lateral trim
    • Bohlmann, J. D., Eckstrom, C. V., and Weisshaar, T. A., "Static Aeroelastic Tailoring for Oblique Wing Lateral Trim," Journal of Aircraft, Vol. 27, No. 6, 1990, pp. 558-563.
    • (1990) Journal of Aircraft , vol.27 , Issue.6 , pp. 558-563
    • Bohlmann, J.D.1    Eckstrom, C.V.2    Weisshaar, T.A.3
  • 15
    • 0024301471 scopus 로고
    • Supersonic flutter of aeroelastically tailored oblique wings
    • Weisshaar, T. A., and Bohlmann, J. D., "Supersonic Flutter of Aeroelastically Tailored Oblique Wings," Journal of Aircraft, Vol. 26, No. 1, 1989, pp. 75-83.
    • (1989) Journal of Aircraft , vol.26 , Issue.1 , pp. 75-83
    • Weisshaar, T.A.1    Bohlmann, J.D.2
  • 16
    • 0020948150 scopus 로고
    • Dynamic stability of flexible forward swept wing aircraft
    • Weisshaar, T. A., and Zeiler, T. A., "Dynamic Stability of Flexible Forward Swept Wing Aircraft," Journal of Aircraft, Vol. 20, No. 12, 1983, pp. 1014-1020.
    • (1983) Journal of Aircraft , vol.20 , Issue.12 , pp. 1014-1020
    • Weisshaar, T.A.1    Zeiler, T.A.2
  • 17
    • 0020799080 scopus 로고
    • Rigid body - Structural mode coupling on a forward swept wing aircraft
    • Miller, G. D., Wykes, J. H., and Brosnan, M. J., "Rigid Body - Structural Mode Coupling on a Forward Swept Wing Aircraft," Journal of Aircraft, Vol. 20, No. 8, 1983, pp. 696-702.
    • (1983) Journal of Aircraft , vol.20 , Issue.8 , pp. 696-702
    • Miller, G.D.1    Wykes, J.H.2    Brosnan, M.J.3
  • 18
    • 0022439360 scopus 로고
    • Control of a forward swept wing configuration dominated by flight dynamics/aeroelastic interactions
    • Rimer, M., Chipman, R., and Muniz, B., "Control of a Forward Swept Wing Configuration Dominated by Flight Dynamics/Aeroelastic Interactions," Journal of Guidance, Control, and Dynamics, Vol. 9, No. 1, 1986, pp. 72-79.
    • (1986) Journal of Guidance, Control, and Dynamics , vol.9 , Issue.1 , pp. 72-79
    • Rimer, M.1    Chipman, R.2    Muniz, B.3
  • 20
    • 0034273883 scopus 로고    scopus 로고
    • Aeroservoelastic analysis of the B-2 bomber
    • Britt, R. T., Jackobson, S. B., and Arthurs, T. D., "Aeroservoelastic Analysis of the B-2 Bomber," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 745-752.
    • (2000) Journal of Aircraft , vol.37 , Issue.5 , pp. 745-752
    • Britt, R.T.1    Jackobson, S.B.2    Arthurs, T.D.3
  • 21
    • 24544443386 scopus 로고    scopus 로고
    • The challenge and promise of blended-wing-body optimization
    • AIAA Paper 98-4736, Sept.
    • Wakayama, S., and Kroo, I., "The Challenge and Promise of Blended-Wing-Body Optimization," AIAA Paper 98-4736, Sept. 1998.
    • (1998)
    • Wakayama, S.1    Kroo, I.2
  • 22
    • 84894330849 scopus 로고    scopus 로고
    • Blended-wing-body optimization problem setup
    • AIAA Paper 2000-4740, Sept.
    • Wakayama, S., "Blended-Wing-Body Optimization Problem Setup," AIAA Paper 2000-4740, Sept. 2000.
    • (2000)
    • Wakayama, S.1
  • 24
    • 0348184915 scopus 로고
    • Preliminary design optimization of joined-wing aircraft
    • Gallman, J., and Kroo, I., "Preliminary Design Optimization of Joined-Wing Aircraft," Journal of Aircraft, No. 6, 1993.
    • (1993) Journal of Aircraft , Issue.6
    • Gallman, J.1    Kroo, I.2
  • 25
    • 0029710536 scopus 로고    scopus 로고
    • Structural optimization for joined-wing synthesis
    • Gallman, J., and Kroo, I., "Structural Optimization for Joined-Wing Synthesis," Journal of Aircraft, Vol. 33, No. 1, 1996, pp. 214-223.
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 214-223
    • Gallman, J.1    Kroo, I.2
  • 26
    • 85067318027 scopus 로고    scopus 로고
    • Aeroelasticity of joined-wing airplane configurations: Past work and future challenges
    • AIAA Paper 2001-1370, April
    • Livne, E., "Aeroelasticity of Joined-Wing Airplane Configurations: Past Work and Future Challenges," AIAA Paper 2001-1370, April 2001.
    • (2001)
    • Livne, E.1
  • 27
    • 0036076288 scopus 로고    scopus 로고
    • Aeroelastic tailoring of joined-wing configurations
    • AIAA Paper 2002-1207, April
    • Weisshaar, T. A., and Lee, D., "Aeroelastic Tailoring of Joined-Wing Configurations," AIAA Paper 2002-1207, April 2002.
    • (2002)
    • Weisshaar, T.A.1    Lee, D.2
  • 28
    • 0035079310 scopus 로고    scopus 로고
    • Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft
    • Patil, M., Hodges, D. H., and Cesnik, C. E. S., "Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft," Journal of Aircraft, Vol. 38, No. 1, 2001, pp. 88-94.
    • (2001) Journal of Aircraft , vol.38 , Issue.1 , pp. 88-94
    • Patil, M.1    Hodges, D.H.2    Cesnik, C.E.S.3
  • 29
    • 0025502974 scopus 로고
    • Aeroelastic characteristics of a highly flexible aircraft
    • Van Schoor, M. C., and von Flotow, A. H., "Aeroelastic Characteristics of a Highly Flexible Aircraft," Journal of Aircraft, Vol. 27, No. 10, 1990, pp. 901-908.
    • (1990) Journal of Aircraft , vol.27 , Issue.10 , pp. 901-908
    • Van Schoor, M.C.1    Von Flotow, A.H.2
  • 30
    • 0032659848 scopus 로고    scopus 로고
    • Integrated model for preliminary aerodynamic, structural, and control-law design of aircraft
    • AIAA Paper 99-1394, April
    • Drela, M., "Integrated Model for Preliminary Aerodynamic, Structural, and Control-Law Design of Aircraft," AIAA Paper 99-1394, April 1999.
    • (1999)
    • Drela, M.1
  • 31
    • 0035421036 scopus 로고    scopus 로고
    • Experimental and theoretical study on the aeroelastic response of high aspect ratio wings
    • Tang, D., and Dowell, E. H., "Experimental and Theoretical Study on the Aeroelastic Response of High Aspect Ratio Wings," AIAA Journal, Vol. 39, No. 8, 2001, pp. 1430-1441.
    • (2001) AIAA Journal , vol.39 , Issue.8 , pp. 1430-1441
    • Tang, D.1    Dowell, E.H.2
  • 32
    • 0034833242 scopus 로고    scopus 로고
    • Effect of angle of attack on nonlinear flutter of a delta wing
    • Tang, D., and Dowell, E. H., "Effect of Angle of Attack on Nonlinear Flutter of a Delta Wing," AIAA Journal, Vol.39, No. 1, 2001, pp. 15-21.
    • (2001) AIAA Journal , vol.39 , Issue.1 , pp. 15-21
    • Tang, D.1    Dowell, E.H.2
  • 34
    • 24544443149 scopus 로고
    • An analysis of the effects of aeroelasticity on the static longitudinal stability and control of a swept-wing airplane
    • NACA Rept. 1298
    • Skoog, R. B., "An Analysis of the Effects of Aeroelasticity on the Static Longitudinal Stability and Control of a Swept-Wing Airplane," NACA Rept. 1298, 1957.
    • (1957)
    • Skoog, R.B.1
  • 35
    • 85007675302 scopus 로고
    • Dihedral effect of a flexible wing
    • Rodden, W. P., "Dihedral Effect of a Flexible Wing," Journal of Aircraft, Vol. 2, No. 5, 1965, pp. 368-373.
    • (1965) Journal of Aircraft , vol.2 , Issue.5 , pp. 368-373
    • Rodden, W.P.1
  • 36
    • 85039572607 scopus 로고
    • Secondary considerations of static aeroelastic effects on high-performance aircraft, static aeroelasticity in combat aircraft
    • AGARD Rept. 725, Jan.
    • Rodden, W. P., "Secondary Considerations of Static Aeroelastic Effects on High-Performance Aircraft, Static Aeroelasticity in Combat Aircraft," AGARD Rept. 725, Jan. 1986.
    • (1986)
    • Rodden, W.P.1
  • 39
    • 0017477959 scopus 로고
    • Effect of stabilizer dihedral and static lift on T-tail flutter
    • Jennings, W. P., and Berry, M. A., "Effect of Stabilizer Dihedral and Static Lift on T-Tail Flutter," Journal of Aircraft, Vol. 14, No. 4, 1977, pp. 364-367.
    • (1977) Journal of Aircraft , vol.14 , Issue.4 , pp. 364-367
    • Jennings, W.P.1    Berry, M.A.2
  • 40
    • 85003413009 scopus 로고
    • Comment on 'effect of stabilizer dihedral and static lift on T-tail flutter
    • Rodden, W. P., "Comment on 'Effect of Stabilizer Dihedral and Static Lift on T-Tail Flutter," Journal of Aircraft, Vol. 15, No. 7, 1978, pp. 447, 448.
    • (1978) Journal of Aircraft , vol.15 , Issue.7 , pp. 447-448
    • Rodden, W.P.1
  • 41
    • 0346294166 scopus 로고    scopus 로고
    • MSC/NASTRAN flutter analysis of T-tails including horizontal stabilizer static lift effects and T-tail transonic dip
    • Suciu, Emil, "MSC/NASTRAN Flutter Analysis of T-Tails Including Horizontal Stabilizer Static Lift Effects and T-Tail Transonic Dip," MSC 1996 World Users' Conference Proceedings, Vol. V, 1996.
    • (1996) MSC 1996 World Users' Conference Proceedings , vol.5
    • Suciu, E.1
  • 42
    • 0242373669 scopus 로고    scopus 로고
    • The development of the doublet lattice method
    • Confederation of European Aerospace Societies, Rome
    • Rodden, W. P., "The Development of the Doublet Lattice Method," International Forum on Aeroelasticity and Structural Dynamics, Vol. II, Confederation of European Aerospace Societies, Rome, 1997, p. 107.
    • (1997) International Forum on Aeroelasticity and Structural Dynamics , vol.2 , pp. 107
    • Rodden, W.P.1
  • 43
    • 85007685430 scopus 로고
    • A doublet lattice method for calculating lift distributions on oscillating surfaces in subsonic flows
    • Albano, E., and Rodden, W. P., "A Doublet Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows," AIAA Journal, Vol. 7, 1969, pp. 279-285.
    • (1969) AIAA Journal , vol.7 , pp. 279-285
    • Albano, E.1    Rodden, W.P.2
  • 44
    • 0015082646 scopus 로고
    • Application of the doublet lattice method to nonplanar configurations in subsonic flow
    • Kalman, T. P., Rodden, W. P., and Giesing, J. P., "Application of the Doublet Lattice Method to Nonplanar Configurations in Subsonic Flow," Journal of Aircraft, Vol. 8, 1971, pp. 406-413.
    • (1971) Journal of Aircraft , vol.8 , pp. 406-413
    • Kalman, T.P.1    Rodden, W.P.2    Giesing, J.P.3
  • 45
    • 0015255754 scopus 로고
    • Refinement of the nonplanar aspects of the subsonic doublet lattice lifting surface method
    • Rodden, W. P., Giesing, J. P., and Kalman, T. P., "Refinement of the Nonplanar Aspects of the Subsonic Doublet Latice Lifting Surface Method," Journal of Aircraft, Vol. 9, 1972, pp. 69-73.
    • (1972) Journal of Aircraft , vol.9 , pp. 69-73
    • Rodden, W.P.1    Giesing, J.P.2    Kalman, T.P.3
  • 46
    • 0014779865 scopus 로고
    • Application of oscillatory aerodynamic theory to estimation of dynamic stability derivatives
    • Rodden, W. P., and Giesing, J. P., "Application of Oscillatory Aerodynamic Theory to Estimation of Dynamic Stability Derivatives," Journal of Aircraft, Vol. 7, No. 3, 1970, pp. 272-275
    • (1970) Journal of Aircraft , vol.7 , Issue.3 , pp. 272-275
    • Rodden, W.P.1    Giesing, J.P.2
  • 47
    • 0344974000 scopus 로고
    • Errata and addenda
    • "Errata and Addenda," Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 93, 94.
    • (1984) Journal of Aircraft , vol.21 , Issue.1 , pp. 93-94
  • 48
    • 85039564323 scopus 로고
    • Dowell, E. H. (ed.); Kluwer Academic, Norwell, MA; Chap. 2
    • Dowell, E. H. (ed.), A Modern Course in Aeroelasticity, 3rd ed., Kluwer Academic, Norwell, MA, 1995, Chap. 2.
    • (1995) A Modern Course in Aeroelasticity, 3rd Ed.
  • 49
    • 85002883358 scopus 로고
    • Development of airplane stability and control technology
    • Perkins, C. D., "Development of Airplane Stability and Control Technology," Journal of Aircraft, Vol. 7, No. 4, 1970, pp. 290-301.
    • (1970) Journal of Aircraft , vol.7 , Issue.4 , pp. 290-301
    • Perkins, C.D.1
  • 50
    • 0346924262 scopus 로고
    • Aeroelastic tailoring for control and performance - Are requirements compatible?
    • AGARD
    • Booker, D., "Aeroelastic Tailoring for Control and Performance - Are Requirements Compatible?," Combat Aircraft Maneuverability, AGARD, 1981.
    • (1981) Combat Aircraft Maneuverability
    • Booker, D.1
  • 52
    • 85039567873 scopus 로고
    • Consistency in aircraft structural and flight control analysis
    • AGARD CP-228, April
    • Schwanz, R. C., "Consistency in Aircraft Structural and Flight Control Analysis," AGARD CP-228, April 1977.
    • (1977)
    • Schwanz, R.C.1
  • 53
    • 24544441956 scopus 로고
    • Nonlinear simulation of a flexible aircraft in maneuvering flight
    • AIAA Paper 87-2501, Aug.
    • Buttrill, C. S., Zeiler, T. A., and Arbuckle, P. D., "Nonlinear Simulation of a Flexible Aircraft in Maneuvering Flight," AIAA Paper 87-2501, Aug. 1987.
    • (1987)
    • Buttrill, C.S.1    Zeiler, T.A.2    Arbuckle, P.D.3
  • 54
    • 0024301591 scopus 로고
    • Integrated aeroservoelastic analysis capability with X-29A comparisons
    • Gupta, K. K., Brenner, M. J., and Voelker, L. S., "Integrated Aeroservoelastic Analysis Capability with X-29A Comparisons," Journal of Aircraft, Vol. 26, No. 1, 1989, pp. 84-90.
    • (1989) Journal of Aircraft , vol.26 , Issue.1 , pp. 84-90
    • Gupta, K.K.1    Brenner, M.J.2    Voelker, L.S.3
  • 55
    • 85002560541 scopus 로고    scopus 로고
    • Towards an integrated approach to the optimum design of actively controlled composite wings
    • Livne, E., Schmit, L. A., and Friedmann, P. P., "Towards an Integrated Approach to the Optimum Design of Actively Controlled Composite Wings," Journal of Aircraft, Vol. 27, No. 6, 1990, pp. 979-992.
    • (1997) Journal of Aircraft , vol.27 , Issue.6 , pp. 979-992
    • Livne, E.1    Schmit, L.A.2    Friedmann, P.P.3
  • 56
    • 0032715079 scopus 로고    scopus 로고
    • Reduced-order models for integrated aeroservoelastic optimization
    • Karpel, M., "Reduced-Order Models for Integrated Aeroservoelastic Optimization," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 146-155.
    • (1999) Journal of Aircraft , vol.36 , Issue.1 , pp. 146-155
    • Karpel, M.1
  • 57
    • 0034273885 scopus 로고    scopus 로고
    • Reduced-order dynamic aeroelastic model development and integration with nonlinear simulation
    • Winther, B. A., Goggin, P. J., and Dykman, J. R., "Reduced-Order Dynamic Aeroelastic Model Development and Integration with Nonlinear Simulation," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 833-839.
    • (2000) Journal of Aircraft , vol.37 , Issue.5 , pp. 833-839
    • Winther, B.A.1    Goggin, P.J.2    Dykman, J.R.3
  • 58
    • 85041690985 scopus 로고
    • The influence of powered controls
    • Chap. 5
    • Benum, D., "The Influence of Powered Controls," AGARD Manual on Aeroelasticity, Pt. I, 1959, Chap. 5.
    • (1959) AGARD Manual on Aeroelasticity , Issue.PART 1
    • Benum, D.1
  • 59
    • 85039569273 scopus 로고
    • The effect of structural deformation on the behavior in flight of a servo-control in association with an automatic pilot
    • Lazennec, H., "The Effect of Structural Deformation on the Behavior in Flight of a Servo-Control in Association with an Automatic Pilot," AGARD Manual on Aeroelasticity, Pt. III, 1968.
    • (1968) AGARD Manual on Aeroelasticity , Issue.PART 3
    • Lazennec, H.1
  • 60
    • 0020765791 scopus 로고
    • Aircraft active controls - New era in design
    • June
    • Hwang, C., and Kesler, D. F., "Aircraft Active Controls - New Era in Design," Astronautics and Aeronautics, June 1983, pp. 70-85.
    • (1983) Astronautics and Aeronautics , pp. 70-85
    • Hwang, C.1    Kesler, D.F.2
  • 61
    • 24544474061 scopus 로고
    • An aeroelastician's perspective of wind tunnel and flight experiences with active control of structural response and stability
    • NASA TM-85761
    • Hansen, Perry W., "An Aeroelastician's Perspective of Wind Tunnel and Flight Experiences with Active Control of Structural Response and Stability," NASA TM-85761, 1984.
    • (1984)
    • Hansen, P.W.1
  • 62
    • 0023421819 scopus 로고
    • Interactions between an aircraft structure and active control systems
    • Freyman, R., "Interactions Between an Aircraft Structure and Active Control Systems," Journal of Guidance, Control, and Dynamics, Vol. 10, No. 5, 1987, pp. 447-452.
    • (1987) Journal of Guidance, Control, and Dynamics , vol.10 , Issue.5 , pp. 447-452
    • Freyman, R.1
  • 63
    • 0007376657 scopus 로고
    • Aeroservoelasticity
    • edited by A. K. Noor and S. L. Venneri, American Society of Mechanical Engineers, New York
    • Noll, T. E., "Aeroservoelasticity," Flight Vehicle Materials, Structures, and Dynamics, Vol. 5, edited by A. K. Noor and S. L. Venneri, American Society of Mechanical Engineers, New York, 1993.
    • (1993) Flight Vehicle Materials, Structures, and Dynamics , vol.5
    • Noll, T.E.1
  • 64
    • 85039584187 scopus 로고
    • Dowell, E. H. (ed.); Kluwer Academic, Norwell, MA; Chap. 12
    • Dowell, E. H. (ed.), A Modern Course in Aeroelasticity, 3rd ed., Kluwer Academic, Norwell, MA, 1995, Chap. 12.
    • (1995) A Modern Course in Aeroelasticity, 3rd Ed.
  • 65
    • 0032756411 scopus 로고    scopus 로고
    • Integrated aeroservoelastic optimization: Status and direction
    • (see p. 139, References by Subject, Aeroservoelasticity of Real Airplanes entry)
    • Livne, E., "Integrated Aeroservoelastic Optimization: Status and Direction," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 122-145 (see p. 139, References by Subject, Aeroservoelasticity of Real Airplanes entry).
    • (1999) Journal of Aircraft , vol.36 , Issue.1 , pp. 122-145
    • Livne, E.1
  • 67
    • 0347555381 scopus 로고
    • YF16 active control system/structural dynamics interaction instability
    • AIAA Paper 75-823, May
    • Peloubet, R. P., "YF16 Active Control System/Structural Dynamics Interaction Instability," AIAA Paper 75-823, May 1975.
    • (1975)
    • Peloubet, R.P.1
  • 68
    • 85017377046 scopus 로고    scopus 로고
    • Aeroservoelastic instability
    • edited by D. D. Liu, D. Sarhaddi, L. S. Wasserman, W. Roberts, R. E. Donham, G. A. Watts, and R. P. Peloubet, Flight Dynamics Directorate, Wright Lab., U. S. Air Force Material Command, WL-TR-96-3111, March
    • Peloubet, R. P., "Aeroservoelastic Instability," Flutter Prevention Handbook: A Preliminary Collection, edited by D. D. Liu, D. Sarhaddi, L. S. Wasserman, W. Roberts, R. E. Donham, G. A. Watts, and R. P. Peloubet, Flight Dynamics Directorate, Wright Lab., U. S. Air Force Material Command, WL-TR-96-3111, March 1997.
    • (1997) Flutter Prevention Handbook: A Preliminary Collection
    • Peloubet, R.P.1
  • 69
    • 85002807968 scopus 로고
    • Limitations of statically unstable aircraft due to the effects of sensor noise, turbulence, and structural dynamics
    • AIAA Paper 86-2203
    • Beaufrere, H., "Limitations of Statically Unstable Aircraft due to the Effects of Sensor Noise, Turbulence, and Structural Dynamics," AIAA Paper 86-2203, 1986.
    • (1986)
    • Beaufrere, H.1
  • 70
    • 24544466684 scopus 로고
    • Impact of aircraft structural dynamics on integrated control design
    • AIAA Paper 83-2216
    • Yamamoto, T., "Impact of Aircraft Structural Dynamics on Integrated Control Design," AIAA Paper 83-2216, 1983.
    • (1983)
    • Yamamoto, T.1
  • 72
    • 0347555372 scopus 로고    scopus 로고
    • The structural coupling resulting from interaction of flight control system and aircraft structure
    • Confederation of European Aerospace Societies
    • Becker, J., "The Structural Coupling Resulting from Interaction of Flight Control System and Aircraft Structure," International Forum on Aeroelasticity and Structural Dynamics, Vol. II, Confederation of European Aerospace Societies, 1997, pp. 241-250.
    • (1997) International Forum on Aeroelasticity and Structural Dynamics , vol.2 , pp. 241-250
    • Becker, J.1
  • 74
    • 0027593711 scopus 로고
    • Integrated structure/control/aerodynamic synthesis of actively controlled composite wings
    • Livne, E., Schmit, L. A., and Friedmann, P. P., "Integrated Structure/Control/Aerodynamic Synthesis of Actively Controlled Composite Wings," Journal of Aircraft, Vol. 30, No. 3, 1993, pp. 387-394.
    • (1993) Journal of Aircraft , vol.30 , Issue.3 , pp. 387-394
    • Livne, E.1    Schmit, L.A.2    Friedmann, P.P.3
  • 75
    • 0032629010 scopus 로고    scopus 로고
    • Aeroservoelastic interaction between aircraft structural and control design schemes
    • Idan, M., Karpel, M., and Moulin, B., "Aeroservoelastic Interaction Between Aircraft Structural and Control Design Schemes," Journal of Guidance, Control, and Dynamics, Vol. 22, No. 4, 1999, pp. 513-519.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.4 , pp. 513-519
    • Idan, M.1    Karpel, M.2    Moulin, B.3
  • 78
    • 0022204420 scopus 로고
    • Active aeroelastic oscillation control on the F/A-18 aircraft
    • AIAA Paper 85-1858, Aug.
    • Trame, L. W., Williams, L. E., and Yurkovich, R. N., "Active Aeroelastic Oscillation Control on the F/A-18 Aircraft," AIAA Paper 85-1858, Aug. 1985.
    • (1985)
    • Trame, L.W.1    Williams, L.E.2    Yurkovich, R.N.3
  • 80
    • 0022593699 scopus 로고
    • Flutter of wings with leading edge control surfaces
    • AIAA Paper 86-0897
    • Yurkovich, R. N., "Flutter of Wings with Leading Edge Control Surfaces," AIAA Paper 86-0897, 1986.
    • (1986)
    • Yurkovich, R.N.1
  • 81
    • 0348184876 scopus 로고    scopus 로고
    • The state of the art of unsteady aerodynamics for high performance aircraft
    • Association de Ingenieros Aeronauticos de Espana, Vol. 1, Madrid, Spain
    • Yurkovich, R., Liu, D. D., and Chen, P. C., "The State of the Art of Unsteady Aerodynamics for High Performance Aircraft," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2001, Vol. 1, Association de Ingenieros Aeronauticos de Espana, Vol. 1, Madrid, Spain, 2001, pp. 47-68.
    • (2001) Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2001 , vol.1 , pp. 47-68
    • Yurkovich, R.1    Liu, D.D.2    Chen, P.C.3
  • 83
    • 0348184881 scopus 로고
    • Flutter of control surfaces and tabs
    • Chap. 3
    • Regier, A. A., "Flutter of Control Surfaces and Tabs," AGARD Manual on Aeroelasticity, Vol. V, 1960, Chap. 3.
    • (1960) AGARD Manual on Aeroelasticity , vol.5
    • Regier, A.A.1
  • 84
    • 0348184877 scopus 로고
    • Flutter of powered controls and of all-miving tailplanes
    • Chap. 4
    • Smith, A. D. N., "Flutter of Powered Controls and of All-Miving Tailplanes," AGARD Manual on Aeroelasticity, Vol. V, 1960, Chap. 4.
    • (1960) AGARD Manual on Aeroelasticity , vol.5
    • Smith, A.D.N.1
  • 85
    • 84911768064 scopus 로고
    • Flutter in one degree of freedom
    • (rev. 1968), Chap. 5
    • Lambourne, N. C., "Flutter in One Degree of Freedom," AGARD Manual on Aeroelasticity, Vol. V, 1960 (rev. 1968), Chap. 5.
    • (1960) AGARD Manual on Aeroelasticity , vol.5
    • Lambourne, N.C.1
  • 87
    • 0348184878 scopus 로고
    • Minimum weight design of the F-15 empennage for flutter
    • AIAA Paper 75-777, April
    • Shelton, J. D., and Tucker, P. B., "Minimum Weight Design of the F-15 Empennage for Flutter," AIAA Paper 75-777, April 1975.
    • (1975)
    • Shelton, J.D.1    Tucker, P.B.2
  • 88
    • 85039571268 scopus 로고    scopus 로고
    • Aerodynamic and mass balance effects on control surface flutter
    • edited by D. D. Liu, D. Sarhaddi, L. S. Wasserman, W. Roberts, R. E. Donham, G. A. Watts, and R. P. Peloubet, Flight Dynamics Directorate, Wright Lab., U.S. Air Force Material Command, WL-TR-96-3111, March
    • Donham, R. E., and Watts, G. A., "Aerodynamic and Mass Balance Effects on Control Surface Flutter," Flutter Prevention Handbook: A Preliminary Collection, edited by D. D. Liu, D. Sarhaddi, L. S. Wasserman, W. Roberts, R. E. Donham, G. A. Watts, and R. P. Peloubet, Flight Dynamics Directorate, Wright Lab., U.S. Air Force Material Command, WL-TR-96-3111, March 1997.
    • (1997) Flutter Prevention Handbook: A Preliminary Collection
    • Donham, R.E.1    Watts, G.A.2
  • 89
    • 85039577000 scopus 로고    scopus 로고
    • Flutter occurrence on eighteen high performance military aircraft
    • edited by D. D. Liu, D. Sarhaddi, L. S. Wasserman, W. Roberts, R. E. Donham, G. A. Watts, and R. P. Peloubet, Flight Dynamics Directorate, Wright Lab., U.S. Air Force Material Command, WL-TR-96-3111, March
    • Roberts, W., "Flutter Occurrence on Eighteen High Performance Military Aircraft," Flutter Prevention Handbook: A Preliminary Collection, edited by D. D. Liu, D. Sarhaddi, L. S. Wasserman, W. Roberts, R. E. Donham, G. A. Watts, and R. P. Peloubet, Flight Dynamics Directorate, Wright Lab., U.S. Air Force Material Command, WL-TR-96-3111, March 1997.
    • (1997) Flutter Prevention Handbook: A Preliminary Collection
    • Roberts, W.1
  • 90
    • 0001935145 scopus 로고
    • An investigation of the effects of certain types of structural nonlinearities on wing and control surface flutter
    • Jan.
    • Woolston, D. S., Runyan, H. L., and Andrews, R. E., "An Investigation of the Effects of Certain Types of Structural Nonlinearities on Wing and Control Surface Flutter," Journal of the Aeronautical Sciences, Vol. 24, Jan. 1957, pp. 57-63
    • (1957) Journal of the Aeronautical Sciences , vol.24 , pp. 57-63
    • Woolston, D.S.1    Runyan, H.L.2    Andrews, R.E.3
  • 92
    • 0022711409 scopus 로고
    • An iterative procedure for non linear flutter analysis
    • Lee, C. L., "An Iterative Procedure for Non Linear Flutter Analysis," AIAA Journal, Vol. 24, No. 5, 1986.
    • (1986) AIAA Journal , vol.24 , Issue.5
    • Lee, C.L.1
  • 93
    • 85095905396 scopus 로고
    • Effects of structural nonlinearities on aircraft vibration and flutter
    • AGARD, R-665
    • Breitbach, E., "Effects of Structural Nonlinearities on Aircraft Vibration and Flutter," AGARD, R-665, 1977.
    • (1977)
    • Breitbach, E.1
  • 94
    • 85039579807 scopus 로고
    • Effects of a non-linear system (free play) on space shuttle body flap modal responses
    • AIAA Paper 95-1254, April
    • Park, C. C., and Misel, J. E., "Effects of a Non-Linear System (Free Play) on Space Shuttle Body Flap Modal Responses," AIAA Paper 95-1254, April 1995.
    • (1995)
    • Park, C.C.1    Misel, J.E.2
  • 96
    • 0041005529 scopus 로고    scopus 로고
    • Flutter prediction on a combat aircraft involving backlash and actuator failures on control surfaces
    • Confederation of European Aerospace Societies
    • Luber, W. G., "Flutter Prediction on a Combat Aircraft Involving Backlash and Actuator Failures on Control Surfaces," International Forum on Aeroelasticity and Structural Dynamics, Vol. II, Confederation of European Aerospace Societies, 1997, pp. 173-182.
    • (1997) International Forum on Aeroelasticity and Structural Dynamics , vol.2 , pp. 173-182
    • Luber, W.G.1
  • 101
    • 0347555374 scopus 로고
    • Nonlinear aeroelasticity
    • edited by A. K. Noor and S. L. Venneri; American Society of Mechanical Engineers, New York; Chap. 4
    • Dowell, E. H. "Nonlinear Aeroelasticity," Flight-Vehicle Materials, Structures, and Dynamics, edited by A. K. Noor and S. L. Venneri, Vol. 5, Pt. II, American Society of Mechanical Engineers, New York, 1993, Chap. 4.
    • (1993) Flight-Vehicle Materials, Structures, and Dynamics , vol.5 , Issue.PART 2
    • Dowell, E.H.1
  • 103
    • 0028730657 scopus 로고
    • Aerodynamic aspects of transonic limit cycle oscillations
    • edited by P. P. Friedmann and J. C. I. Chang, American Society of Mechanical Engineers, New York
    • Cunningham, A. M., Jr., "Aerodynamic Aspects of Transonic Limit Cycle Oscillations," Aeroelasticity and Fluid Structure Interaction Problems, AD-Vol. 44, edited by P. P. Friedmann and J. C. I. Chang, American Society of Mechanical Engineers, New York, 1994, pp. 29-47.
    • (1994) Aeroelasticity and Fluid Structure Interaction Problems , vol.AD-Vol. 44 , pp. 29-47
    • Cunningham Jr., A.M.1
  • 104
    • 0041416606 scopus 로고
    • Computational aeroelasticity
    • edited by A. K. Noor and S. L. Venneri, American Society of Mechanical Engineerings, New York
    • Edwards, J. W., "Computational Aeroelasticity," Flight Vehicle Materials, Structures, and Dynamics, Vol. 5, edited by A. K. Noor and S. L. Venneri, American Society of Mechanical Engineerings, New York, 1993.
    • (1993) Flight Vehicle Materials, Structures, and Dynamics , vol.5
    • Edwards, J.W.1
  • 105
    • 0007421323 scopus 로고    scopus 로고
    • An overview of recent developments in computational aeroelasticity
    • AIAA Paper 98-2421, June
    • Bennet, R. M., and Edwards, J. W., "An Overview of Recent Developments in Computational Aeroelasticity," AIAA Paper 98-2421, June 1998.
    • (1998)
    • Bennet, R.M.1    Edwards, J.W.2
  • 107
    • 0042176896 scopus 로고    scopus 로고
    • Evaluation of computational aeroelasticity codes for loads and flutter
    • AIAA Paper 2001-0569, Jan.
    • Huttsell, L., Schuster, D., Volk, J., Giesing, J., and Love, M., "Evaluation of Computational Aeroelasticity Codes for Loads and Flutter," AIAA Paper 2001-0569, Jan. 2001.
    • (2001)
    • Huttsell, L.1    Schuster, D.2    Volk, J.3    Giesing, J.4    Love, M.5
  • 108
    • 0035272350 scopus 로고    scopus 로고
    • Navier-stokes computations of limit-cycle oscillations for a B-1 like configuration
    • Hartwich, P. M., Dobbs, S. K., Arslan, A. E., and Kim, S. C., "Navier-Stokes Computations of Limit-Cycle Oscillations for a B-1 Like Configuration," Journal of Aircraft, Vol. 38, No. 2, 2001, pp. 239-247.
    • (2001) Journal of Aircraft , vol.38 , Issue.2 , pp. 239-247
    • Hartwich, P.M.1    Dobbs, S.K.2    Arslan, A.E.3    Kim, S.C.4
  • 109
    • 0036575675 scopus 로고    scopus 로고
    • Comment on Navier-Stokes computations of limit-cycle oscillations for a B-1 like configuration
    • Ericsson, L. E., "Comment on Navier-Stokes Computations of Limit-Cycle Oscillations for a B-1 Like Configuration," Journal of Aircraft, Vol. 39, No. 3, 2002, p. 519.
    • (2002) Journal of Aircraft , vol.39 , Issue.3 , pp. 519
    • Ericsson, L.E.1
  • 110
    • 0036575688 scopus 로고    scopus 로고
    • Reply to comment on Navier-Stokes computations of limit-cycle oscillations for a B-1 like configuration
    • Hartwich, P. M., Dobbs, S. K., Arslan, A. E., and Kim, S. C., "Reply to Comment on Navier-Stokes Computations of Limit-Cycle Oscillations for a B-1 Like Configuration," Journal of Aircraft, Vol. 39, No. 3, 2002, pp. 519, 520.
    • (2002) Journal of Aircraft , vol.39 , Issue.3 , pp. 519-520
    • Hartwich, P.M.1    Dobbs, S.K.2    Arslan, A.E.3    Kim, S.C.4
  • 111
    • 0012958215 scopus 로고
    • Numerical simulations of dynamic/aerodynamic interactions
    • Mook, D. T., and Nayfeh, A. H., "Numerical Simulations of Dynamic/Aerodynamic Interactions," Computing Systems in Engineering, Vol. 1, Nos. 2-4, 1990, pp. 461-482.
    • (1990) Computing Systems in Engineering , vol.1 , Issue.2-4 , pp. 461-482
    • Mook, D.T.1    Nayfeh, A.H.2
  • 112
    • 0012590161 scopus 로고    scopus 로고
    • Nonlinear simulation of F-16 aeroelastic instability
    • AIAA Paper 2001-0570, Jan.
    • Melville, R., "Nonlinear Simulation of F-16 Aeroelastic Instability," AIAA Paper 2001-0570, Jan. 2001.
    • (2001)
    • Melville, R.1
  • 113
    • 0036390834 scopus 로고    scopus 로고
    • Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
    • Farhat, C., Geuzaine, P., and Brown, G., "Application of a Three-Field Nonlinear Fluid-Structure Formulation to the Prediction of the Aeroelastic Parameters of an F-16 Fighter," Computers and Fluids, Vol. 32, 2003, pp. 3-29.
    • (2003) Computers and Fluids , vol.32 , pp. 3-29
    • Farhat, C.1    Geuzaine, P.2    Brown, G.3
  • 114
    • 0042176899 scopus 로고    scopus 로고
    • Nonlinear flutter analysis of an F-16 in stabilized, accelerated, and increased angle of attack flight conditions
    • AIAA Paper 2002-1490, April
    • Farhat, C., Geuzaine, P., Brown, G., and Harris, C., "Nonlinear Flutter Analysis of an F-16 in Stabilized, Accelerated, and Increased Angle of Attack Flight Conditions," AIAA Paper 2002-1490, April 2002.
    • (2002)
    • Farhat, C.1    Geuzaine, P.2    Brown, G.3    Harris, C.4
  • 115
    • 0242373651 scopus 로고    scopus 로고
    • Expanding a flutter envelope using accelerated flight data - Application to an F16 fighter configuration
    • AIAA Paper 2000-1702, April
    • Farhat, C., Harris, C., and Rixen, D. J., "Expanding a Flutter Envelope Using Accelerated Flight Data - Application to an F16 Fighter Configuration," AIAA Paper 2000-1702, April 2000.
    • (2000)
    • Farhat, C.1    Harris, C.2    Rixen, D.J.3
  • 116
    • 85003340183 scopus 로고
    • Comment on 'canard wing interaction in unsteady supersonic flow
    • Johnson, E. H., Rodden, W. P., Chen, P. C., and Liu, D. D., "Comment on 'Canard Wing Interaction in Unsteady Supersonic Flow,'" Journal of Aircraft, Vol. 29, No. 4, 1992, p. 744.
    • (1992) Journal of Aircraft , vol.29 , Issue.4 , pp. 744
    • Johnson, E.H.1    Rodden, W.P.2    Chen, P.C.3    Liu, D.D.4
  • 117
    • 0008485750 scopus 로고
    • Innovation in aircraft structures - Fifty years ago and today
    • AIAA Paper 84-0840, May
    • Hoff, N. J., "Innovation in Aircraft Structures - Fifty Years Ago and Today," AIAA Paper 84-0840, May 1984.
    • (1984)
    • Hoff, N.J.1
  • 118
    • 0021654639 scopus 로고
    • Structural optimization - Some key ideas and insights
    • edited by E. Atrek, R. H. Gallagher, K. M. Ragsdell, and O. C. Zienkiewicz, Wiley, New York
    • Schmit, L. A., Jr., "Structural Optimization - Some Key Ideas and Insights," New Directions in Optimum Structural Design, edited by E. Atrek, R. H. Gallagher, K. M. Ragsdell, and O. C. Zienkiewicz, Wiley, New York, 1984.
    • (1984) New Directions in Optimum Structural Design
    • Schmit Jr., L.A.1
  • 122
    • 0344786436 scopus 로고
    • Automated design of advanced composite structures
    • edited by Zvi Hashin, Pergamon
    • McCullers, L. A., "Automated Design of Advanced Composite Structures," Mechanics of Composite Materials, edited by Zvi Hashin, Pergamon, 1983.
    • (1983) Mechanics of Composite Materials
    • McCullers, L.A.1
  • 123
    • 0022544782 scopus 로고
    • Aeroelatic tailoring - Theory, practice, promise
    • Shirk, M. H., Hertz, T. J., and Weisshaar, T. A., "Aeroelatic Tailoring - Theory, Practice, Promise," Journal of Aircraft, Vol. 23, No. 1, 1986, pp. 6-18.
    • (1986) Journal of Aircraft , vol.23 , Issue.1 , pp. 6-18
    • Shirk, M.H.1    Hertz, T.J.2    Weisshaar, T.A.3
  • 124
    • 0342438553 scopus 로고
    • Aeroelastic tailoring - Creative uses of unusual materials
    • AIAA Paper 87-0976, April
    • Weisshaar, T. A., "Aeroelastic Tailoring - Creative Uses of Unusual Materials," AIAA Paper 87-0976, April 1987.
    • (1987)
    • Weisshaar, T.A.1
  • 125
    • 0023364175 scopus 로고
    • Optimum flap schedules and minimum drag envelopes for combat aircraft
    • Rajeswari, B., and Prabhu, K. R., "Optimum Flap Schedules and Minimum Drag Envelopes for Combat Aircraft," Journal of Aircraft, Vol. 24, No. 6, 1987, pp. 412-414.
    • (1987) Journal of Aircraft , vol.24 , Issue.6 , pp. 412-414
    • Rajeswari, B.1    Prabhu, K.R.2
  • 126
    • 0024055301 scopus 로고
    • GENMAP - Computer code for mission adaptive profile generation
    • Gupta, S. C., "GENMAP - Computer Code for Mission Adaptive Profile Generation," Journal of Aircraft, Vol. 25, No. 8, 1988, pp. 766-768.
    • (1988) Journal of Aircraft , vol.25 , Issue.8 , pp. 766-768
    • Gupta, S.C.1
  • 127
    • 20344393833 scopus 로고    scopus 로고
    • Some applications of active aeroelasticity concept to aircraft design
    • Association de Ingenieros Aeronauticos de Espana, Madrid, Spain
    • Kuzmina, S., Amiryants, G. A., Ishmuratov, F. Z., Mosunov, V. A., and Chedrik, V. V., "Some Applications of Active Aeroelasticity Concept to Aircraft Design," IFASD 2001, Association de Ingenieros Aeronauticos de Espana, Madrid, Spain, 2001.
    • (2001) IFASD 2001
    • Kuzmina, S.1    Amiryants, G.A.2    Ishmuratov, F.Z.3    Mosunov, V.A.4    Chedrik, V.V.5
  • 129
    • 85039576671 scopus 로고
    • The C-5A active lift distribution control system
    • AGARD CP-157, Paper 24
    • Grosser, W. F., Hollenbeck, W. W., and Eckholdt, D. C., "The C-5A Active Lift Distribution Control System," AGARD CP-157, Paper 24, 1974.
    • (1974)
    • Grosser, W.F.1    Hollenbeck, W.W.2    Eckholdt, D.C.3
  • 130
    • 0026617486 scopus 로고
    • The use of variable camber to reduce drag, weight, and costs of transport aircraft
    • Spillman, J. J., "The Use of Variable Camber to Reduce Drag, Weight, and Costs of Transport Aircraft," Aeronautical Journal, Vol. 96, No. 951, 1992, pp. 1-9.
    • (1992) Aeronautical Journal , vol.96 , Issue.951 , pp. 1-9
    • Spillman, J.J.1
  • 131
    • 0005862258 scopus 로고
    • An active flexible wing multidisciplinary design optimization method
    • AIAA Paper 94-4412
    • Miller, G. D., "An Active Flexible Wing Multidisciplinary Design Optimization Method," AIAA Paper 94-4412, 1994.
    • (1994)
    • Miller, G.D.1
  • 132
    • 0026869470 scopus 로고
    • Application of active flexible wing technology to the agile falcon
    • Pendelton, E., Lee, M., and Wasserman, L., "Application of Active Flexible Wing Technology to the Agile Falcon," Journal of Aircraft, Vol. 29, No. 3, 1992, pp. 444-451.
    • (1992) Journal of Aircraft , vol.29 , Issue.3 , pp. 444-451
    • Pendelton, E.1    Lee, M.2    Wasserman, L.3
  • 133
    • 0034226416 scopus 로고    scopus 로고
    • Active aeroelastic wing flight research program: Technical program and model analytical development
    • Pendelton, E. W., Bessette, D., Field, P. B., Miller, G. D., and Griffin, K. E., "Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development," Journal of Aircraft, Vol. 37, No. 4, 2000, pp. 554-561.
    • (2000) Journal of Aircraft , vol.37 , Issue.4 , pp. 554-561
    • Pendelton, E.W.1    Bessette, D.2    Field, P.B.3    Miller, G.D.4    Griffin, K.E.5
  • 134
    • 85003273829 scopus 로고
    • Active flexible wing program - Editorial
    • Noll, T. E., and Eastep, F. E., "Active Flexible Wing Program - Editorial," Journal of Aircraft, Vol. 32, No. 1, 1995, p. 9.
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 9
    • Noll, T.E.1    Eastep, F.E.2
  • 135
    • 0029219120 scopus 로고
    • Summary of an active flexible wing program
    • Perry, B. I., Cole, S. R., and Miller, G. D., "Summary of an Active Flexible Wing Program," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 9-15.
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 9-15
    • Perry, B.I.1    Cole, S.R.2    Miller, G.D.3
  • 136
    • 0004024952 scopus 로고
    • Integrated multidisciplinary optimization of actively controlled fiber composite wings
    • Ph.D. Dissertation, Dept. of Mechanical, Aerospace, and Nuclear Engineering, Univ. of California, Los Angeles
    • Livne, E., "Integrated Multidisciplinary Optimization of Actively Controlled Fiber Composite Wings," Ph.D. Dissertation, Dept. of Mechanical, Aerospace, and Nuclear Engineering, Univ. of California, Los Angeles, 1990.
    • (1990)
    • Livne, E.1
  • 137
    • 24544449110 scopus 로고
    • Aeroelastic consideration in the design of variable sweep aeroplanes
    • International Council of the Aeronautical Sciences, Paper 66-12
    • Topp, L. J., Rowe, W. S., and Shattuck, A. W., "Aeroelastic Consideration in the Design of Variable Sweep Aeroplanes," International Council of the Aeronautical Sciences, Paper 66-12, 1966.
    • (1966)
    • Topp, L.J.1    Rowe, W.S.2    Shattuck, A.W.3
  • 138
    • 85002777339 scopus 로고
    • Flutter induced by aerodynamic interference between wing and tail
    • Sensburg, O., and Laschka, B., "Flutter Induced by Aerodynamic Interference Between Wing and Tail," Journal of Aircraft, Vol. 7, No. 4, 1970, pp. 319-324.
    • (1970) Journal of Aircraft , vol.7 , Issue.4 , pp. 319-324
    • Sensburg, O.1    Laschka, B.2
  • 139
    • 85039584271 scopus 로고
    • A parametric study of wing store flutter
    • AGARD Conference Proceedings No. 162; Chap. 7
    • Chesta, L., "A Parametric Study of Wing Store Flutter," AGARD Conference Proceedings No. 162, 1975, Chap. 7.
    • (1975)
    • Chesta, L.1
  • 140
    • 0347555371 scopus 로고    scopus 로고
    • In-flight transport performance optimization: An experimental flight test research program and an operational scenarion
    • NASA-TM-206229, Oct.
    • Gilyard, G., "In-Flight Transport Performance Optimization: An Experimental Flight Test Research Program and an Operational Scenarion," NASA-TM-206229, Oct. 1997.
    • (1997)
    • Gilyard, G.1
  • 141
    • 0002726762 scopus 로고
    • Flight test results from a supercritical mission adaptive wing with Smooth variable camber
    • NASA TM-4415, Nov.
    • Powers, S. G., Webb, L. D., Friend, E. L., and Lokos, W. A., "Flight Test Results from a Supercritical Mission Adaptive Wing with Smooth Variable Camber," NASA TM-4415, Nov. 1992.
    • (1992)
    • Powers, S.G.1    Webb, L.D.2    Friend, E.L.3    Lokos, W.A.4
  • 142
    • 0006340092 scopus 로고
    • Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI)/F-111 mission adaptive wing
    • NASA TM-4526, Sept.
    • Thornton, S. V., "Reduction of Structural Loads Using Maneuver Load Control on the Advanced Fighter Technology Integration (AFTI)/F-111 Mission Adaptive Wing," NASA TM-4526, Sept. 1993.
    • (1993)
    • Thornton, S.V.1
  • 143
    • 0346294156 scopus 로고
    • Advanced fighter technology integration F-111 mission adaptive wing
    • NASA CP 3055
    • "Advanced Fighter Technology Integration F-111 Mission Adaptive Wing," NASA CP 3055, 1989.
    • (1989)
  • 144
    • 0018051910 scopus 로고
    • Some observations on four current subjects related to aeroelastic stability
    • Ashley, H., "Some Observations on Four Current Subjects Related to Aeroelastic Stability," Israel Journal of Technology, Vol. 16, 1978, pp. 3-22.
    • (1978) Israel Journal of Technology , vol.16 , pp. 3-22
    • Ashley, H.1
  • 145
    • 0017013512 scopus 로고
    • Drag effects on wing flutter
    • Petre, A., and Ashley, H., "Drag Effects on Wing Flutter," Journal of Aircraft, Vol. 13, 1976, pp. 755-763.
    • (1976) Journal of Aircraft , vol.13 , pp. 755-763
    • Petre, A.1    Ashley, H.2
  • 146
    • 85002859747 scopus 로고
    • Effects of chordwise forces and deformations due to steady lift on wing flutter
    • Ph.D. Dissertation, SUDAAR No. 508, Dept. of Aeronautics and Astronautics, Stanford Univ., CA
    • Boyd, W. N., "Effects of Chordwise Forces and Deformations due to Steady Lift on Wing Flutter," Ph.D. Dissertation, SUDAAR No. 508, Dept. of Aeronautics and Astronautics, Stanford Univ., CA, 1977.
    • (1977)
    • Boyd, W.N.1
  • 147
    • 85039563643 scopus 로고
    • Aerodynamic interference: Papers presented at a specialists' meeting of the fluid dynamic panel of AGARD
    • Silver Spring, MD, Sept. 1970; AGARD Conference Proceedings No. 71, NATO, Paris
    • "Aerodynamic Interference: Papers Presented at a Specialists' Meeting of the Fluid Dynamic Panel of AGARD," Silver Spring, MD, Sept. 1970; AGARD Conference Proceedings No. 71, NATO, Paris, 1970.
    • (1970)
  • 148
    • 0016129119 scopus 로고
    • Oscillatory supersonic kernel function method for interfering surfaces
    • Cunningham, A. M., "Oscillatory Supersonic Kernel Function Method for Interfering Surfaces," Journal of Aircraft, Vol. 11, No. 11, 1974, pp. 664-670.
    • (1974) Journal of Aircraft , vol.11 , Issue.11 , pp. 664-670
    • Cunningham, A.M.1
  • 149
    • 0347555364 scopus 로고
    • A comparison of methods used in interfering lifting surface theory
    • AGARD, Rept. R-643, March
    • Rodden, W. P., "A Comparison of Methods Used in Interfering Lifting Surface Theory," AGARD, Rept. R-643, March 1976.
    • (1976)
    • Rodden, W.P.1
  • 150
    • 0019560409 scopus 로고
    • Three dimensional oscillatory piecewise continuous kernel function method
    • (in three parts)
    • Lottati, I., and Nissim, E., "Three Dimensional Oscillatory Piecewise Continuous Kernel Function Method" (in three parts), Journal of Aircraft, Vol. 18, No. 5, 1981, pp. 346-363.
    • (1981) Journal of Aircraft , vol.18 , Issue.5 , pp. 346-363
    • Lottati, I.1    Nissim, E.2
  • 151
    • 0346294159 scopus 로고
    • Comparison of analysis methods used in lifting surface theory
    • edited by L. Morino, Springer-Verlag
    • Rowe, W. S., "Comparison of Analysis Methods Used in Lifting Surface Theory," Computational Methods in Potential Aerodynamics, edited by L. Morino, Springer-Verlag, 1985.
    • (1985) Computational Methods in Potential Aerodynamics
    • Rowe, W.S.1
  • 152
    • 0348184873 scopus 로고    scopus 로고
    • Smart air and space structures
    • edited by A. K. Noor, Progress in Aeronautics and Astronautics, AIAA, Reston, VA
    • Sater, J. M., Crowe, C. R., Antcliff, R., and Das, A., "Smart Air and Space Structures," Structures Technology for Future Aerospace Systems, edited by A. K. Noor, Progress in Aeronautics and Astronautics, AIAA, Reston, VA, 2000, pp. 269-350.
    • (2000) Structures Technology for Future Aerospace Systems , pp. 269-350
    • Sater, J.M.1    Crowe, C.R.2    Antcliff, R.3    Das, A.4
  • 153
    • 85039583444 scopus 로고    scopus 로고
    • Exploiting smart technologies for military aircraft applications: Perspectives on development of a smart air vehicle
    • AIAA Paper 99-1511, April
    • Kudva, J. N., and Lockyer, A. J., "Exploiting Smart Technologies for Military Aircraft Applications: Perspectives on Development of a Smart Air Vehicle," AIAA Paper 99-1511, April 1999.
    • (1999)
    • Kudva, J.N.1    Lockyer, A.J.2
  • 154
    • 0028485223 scopus 로고
    • Intelligent structures for aerospace: A technology overview and assessment
    • Crawley, E. F., "Intelligent Structures for Aerospace: A Technology Overview and Assessment," Journal of Aircraft, Vol. 32, No. 8, 1994, pp. 1689-1699.
    • (1994) Journal of Aircraft , vol.32 , Issue.8 , pp. 1689-1699
    • Crawley, E.F.1
  • 156
    • 0036030424 scopus 로고    scopus 로고
    • Recent results for NASA's morphing project
    • Society of Photo-Optical Instrumentation Engineers, Paper 4698-11, March
    • McGowan, A. R., Washburn, A. E., Horta, L. G., Bryant, R. G.; Cox, D. E., Siochi, E. J., Padula, S. L., and Holloway, N. M., "Recent Results for NASA's Morphing Project," Society of Photo-Optical Instrumentation Engineers, Paper 4698-11, March 2002.
    • (2002)
    • McGowan, A.R.1    Washburn, A.E.2    Horta, L.G.3    Bryant, R.G.4    Cox, D.E.5    Siochi, E.J.6    Padula, S.L.7    Holloway, N.M.8
  • 157
    • 85088760784 scopus 로고    scopus 로고
    • Use of design methods to generate and develop missions for morphing aircraft
    • AIAA Paper 2002-5468
    • Peters, C., Roth, B., Crossley, W. A., and Weisshaar, T. A., "Use of Design Methods to Generate and Develop Missions for Morphing Aircraft," AIAA Paper 2002-5468, 2002.
    • (2002)
    • Peters, C.1    Roth, B.2    Crossley, W.A.3    Weisshaar, T.A.4
  • 158
    • 0028733443 scopus 로고    scopus 로고
    • Aeroservoelastic control concepts with active materials
    • edited by P. P. Friedmann and J. C. I. Chang, American Society of Mechanical Engineers
    • Weisshaar, T. A., "Aeroservoelastic Control Concepts with Active Materials," Aeroelasticity and Fluid Structure Interaction Problems, AD-Vol. 44, edited by P. P. Friedmann and J. C. I. Chang, American Society of Mechanical Engineers, pp. 125-146.
    • Aeroelasticity and Fluid Structure Interaction Problems , vol.AD-VOL. 44 , pp. 125-146
    • Weisshaar, T.A.1
  • 160
    • 0031246157 scopus 로고    scopus 로고
    • Recent developments in smart structures with aeronautical applications
    • Oct.
    • Loewy, R. G., "Recent Developments in Smart Structures with Aeronautical Applications," Journal of Smart Materials and Structures, Vol. 5, Oct. 1997, pp. 11-41.
    • (1997) Journal of Smart Materials and Structures , vol.5 , pp. 11-41
    • Loewy, R.G.1
  • 161
    • 0005084716 scopus 로고    scopus 로고
    • A critical review of efforts and achievements to improve aircraft performance or efficiency by active structures concepts
    • Confederation of European Aerospace Societies, Madrid, Spain
    • Schweiger, J., and Sensburg, O., "A Critical Review of Efforts and Achievements to Improve Aircraft Performance or Efficiency by Active Structures Concepts," IFASD 2001, the CEAS/AIAA/AIAE International Forum on Aeroelasticity and Structural Dynamics, Vol. II, Confederation of European Aerospace Societies, Madrid, Spain, 2001, pp. 447-461.
    • (2001) IFASD 2001, the CEAS/AIAA/AIAE International Forum on Aeroelasticity and Structural Dynamics , vol.2 , pp. 447-461
    • Schweiger, J.1    Sensburg, O.2
  • 163
    • 0346924244 scopus 로고
    • Flight investigation of XB-70 structural response to oscillatory aerodynamic shaker excitation and correlation with analytical results
    • NASA-TN-D-7227, April
    • McKay, J. M., Kordes, E. E., and Wykes, J. H., "Flight Investigation of XB-70 Structural Response to Oscillatory Aerodynamic Shaker Excitation and Correlation with Analytical Results," NASA-TN-D-7227, April 1973.
    • (1973)
    • McKay, J.M.1    Kordes, E.E.2    Wykes, J.H.3
  • 164
    • 46149149399 scopus 로고
    • Analytical design and flight tests of a mode suppression system on the XB-70 airplane, Parts I and II
    • Wykes, J. H., and Kordes, J. H., "Analytical Design and Flight Tests of a Mode Suppression System on the XB-70 Airplane, Parts I and II," Aeroelastic Effects from a Flight Mechanics Standpoint, 1970, pp. 23-1-23-18.
    • (1970) Aeroelastic Effects from a Flight Mechanics Standpoint
    • Wykes, J.H.1    Kordes, J.H.2
  • 166
    • 0346294146 scopus 로고
    • Flutter prevention in design of the SST
    • edited by G. Herrmann, and N. Perrone, Pergamon, New York
    • Turner, M. J., and Bartley, J. B., "Flutter Prevention in Design of the SST," Dynamic Response of Structures, edited by G. Herrmann, and N. Perrone, Pergamon, New York, 1972, pp. 95-113.
    • (1972) Dynamic Response of Structures , pp. 95-113
    • Turner, M.J.1    Bartley, J.B.2
  • 167
    • 0347555422 scopus 로고
    • Aeroelastic challenges for a high speed civil transport
    • AIAA Paper 93-1478
    • Bhatia, K. G., and Wertheimer, J., "Aeroelastic Challenges for a High Speed Civil Transport," AIAA Paper 93-1478, 1993.
    • (1993)
    • Bhatia, K.G.1    Wertheimer, J.2
  • 168
    • 0025211319 scopus 로고
    • Experimental transonic flutter characteristics of supersonic cruise configurations
    • AIAA Paper 90-0979
    • Durham, H. M., Cole, S. R., Cazier, F. W., Jr., Keller, D. F., Parker, E. C., and Wilkie, W. K., "Experimental Transonic Flutter Characteristics of Supersonic Cruise Configurations," AIAA Paper 90-0979, 1990.
    • (1990)
    • Durham, H.M.1    Cole, S.R.2    Cazier Jr., F.W.3    Keller, D.F.4    Parker, E.C.5    Wilkie, W.K.6
  • 169
    • 0347555367 scopus 로고    scopus 로고
    • Study on transonic flutter characteristics of an arrow wing configuration
    • Confederation of European Aerospace Socieities
    • Isogai, K., "Study on Transonic Flutter Characteristics of an Arrow Wing Configuration," International Forum on Aeroelasticity and Structural Dynamics, Vol. II, Confederation of European Aerospace Socieities, 1997, pp. 87-95.
    • (1997) International Forum on Aeroelasticity and Structural Dynamics , vol.2 , pp. 87-95
    • Isogai, K.1
  • 170
    • 0346924241 scopus 로고    scopus 로고
    • Measurements of unsteady pressure distribution and dynamic deformatioons on an SST elastic wing model
    • Confederation of European Aerospace Socieities
    • Tamayama, M., Saitoh, K., Matsushita, H., and Nakamichi, J., "Measurements of Unsteady Pressure Distribution and Dynamic Deformatioons on an SST Elastic Wing Model," International Forum on Aeroelasticity and Structural Dynamics, Vol. III, Confederation of European Aerospace Socieities, 1997, pp. 231-238.
    • (1997) International Forum on Aeroelasticity and Structural Dynamics , vol.3 , pp. 231-238
    • Tamayama, M.1    Saitoh, K.2    Matsushita, H.3    Nakamichi, J.4
  • 171
    • 85039572691 scopus 로고    scopus 로고
    • Application of direct search method to aeroelastic tailoring of an arrow wing configuration
    • CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
    • Isogai, K., "Application of Direct Search Method to Aeroelastic Tailoring of an Arrow Wing Configuration," CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999, Pt. 2, pp. 691-697.
    • , Issue.PART 2 , pp. 691-697
    • Isogai, K.1
  • 173
    • 85017343501 scopus 로고
    • The impact of structural vibrations on flying qualities of a supersonic transport
    • AIAA Paper 2001-4006, Aug.
    • Rainey, D. L., Jackson, E. B., Buttrill, C. S., and Adams, W. M., "The Impact of Structural Vibrations on Flying Qualities of a Supersonic Transport," AIAA Paper 2001-4006, Aug. 1991.
    • (1991)
    • Rainey, D.L.1    Jackson, E.B.2    Buttrill, C.S.3    Adams, W.M.4
  • 175
    • 0346924247 scopus 로고
    • Structural heating experiences on the X-15 Airplane
    • NASA TM X-711
    • Kordes, E. E., Reed, R. D., and Dawdy, A. L., "Structural Heating Experiences on the X-15 Airplane," NASA TM X-711, 1962.
    • (1962)
    • Kordes, E.E.1    Reed, R.D.2    Dawdy, A.L.3
  • 176
    • 0347555366 scopus 로고
    • Structural dynamic experiences of the X-15 airplane
    • NASA TN D-1158
    • Jordan, G. H., McLeod, N. J., and Guy, L. D., "Structural Dynamic Experiences of the X-15 Airplane," NASA TN D-1158, 1962.
    • (1962)
    • Jordan, G.H.1    McLeod, N.J.2    Guy, L.D.3
  • 177
    • 0141913340 scopus 로고
    • A survey of aerothermoelasticity
    • Jan.
    • Garrick, I. E., "A Survey of Aerothermoelasticity," Aerospace Engineering, Jan. 1963, pp. 140-147.
    • (1963) Aerospace Engineering , pp. 140-147
    • Garrick, I.E.1
  • 179
    • 0042790068 scopus 로고
    • Some structural and aeroelastic considerations of high speed flight
    • Bisplinghoff, R. L., "Some Structural and Aeroelastic Considerations of High Speed Flight," Journal of the Aerospace Sciences, Vol. 23, No. 4, 1956.
    • (1956) Journal of the Aerospace Sciences , vol.23 , Issue.4
    • Bisplinghoff, R.L.1
  • 180
    • 0348184869 scopus 로고
    • Dynamic and aeroelastic problems of lifting re-entry bodies
    • Jan.
    • Hedgepeth, J., and Widmayer, E., Jr., "Dynamic and Aeroelastic Problems of Lifting Re-Entry Bodies," Aerospace Engineering, Jan. 1963, pp. 148-153.
    • (1963) Aerospace Engineering , pp. 148-153
    • Hedgepeth, J.1    Widmayer Jr., E.2
  • 181
    • 0346294150 scopus 로고
    • Potential aerothermoelastic problems associated with advanced vehicle design
    • Jan.
    • Laidlaw, W. R., and Wykes, J. H., "Potential Aerothermoelastic Problems Associated with Advanced Vehicle Design," Aerospace Engineering, Jan. 1963, pp. 154-164.
    • (1963) Aerospace Engineering , pp. 154-164
    • Laidlaw, W.R.1    Wykes, J.H.2
  • 182
    • 0000051591 scopus 로고
    • Piston theory - A new aerodynamic tool for the aeroelastician
    • Ashley, H., and Zartarian, G., "Piston Theory - A New Aerodynamic Tool for the Aeroelastician," Journal of the Aeronautical Sciences, Vol. 23, No. 12, 1956, pp. 1109-1118.
    • (1956) Journal of the Aeronautical Sciences , vol.23 , Issue.12 , pp. 1109-1118
    • Ashley, H.1    Zartarian, G.2
  • 183
    • 0346294147 scopus 로고    scopus 로고
    • A historical perspective of the YF-12 thermal loads and structures program
    • NASA TM-104317, May
    • Jenkins, J. M., and Quinn, R. D., "A Historical Perspective of the YF-12 Thermal Loads and Structures Program," NASA TM-104317, May 1996.
    • (1996)
    • Jenkins, J.M.1    Quinn, R.D.2
  • 184
    • 85039586959 scopus 로고    scopus 로고
    • Flutter analysis of the linear aerospike SR-71 experiment (LASRE)
    • AIAA Paper 96-1197, April
    • Goforth, A. E., "Flutter Analysis of the Linear Aerospike SR-71 Experiment (LASRE)," AIAA Paper 96-1197, April 1996.
    • (1996)
    • Goforth, A.E.1
  • 185
    • 0348184871 scopus 로고
    • Space shuttle - A new arena for the structural dynamicist
    • edited by G. Hermann and N. Perrone, Pergamon, New York
    • Runyan, H. L., and Goetz, R. C., "Space Shuttle - A New Arena for the Structural Dynamicist," Dynamic Response of Structures, edited by G. Hermann and N. Perrone, Pergamon, New York, 1972.
    • (1972) Dynamic Response of Structures
    • Runyan, H.L.1    Goetz, R.C.2
  • 186
    • 85039581746 scopus 로고
    • Aerothermoelastic stability of a wing
    • Sec. 8.13, MSC/NASTRAN Aeroelastic Analysis User's Guide, Ver. 68, MacNeal-Schwendler Corp.
    • Rodden, W. P., and Johnson, E. H., "Aerothermoelastic Stability of a Wing," Sec. 8.13, MSC/NASTRAN Aeroelastic Analysis User's Guide, Ver. 68, MacNeal-Schwendler Corp., 1994, pp. 551-558.
    • (1994) , pp. 551-558
    • Rodden, W.P.1    Johnson, E.H.2
  • 188
    • 0347555365 scopus 로고
    • NASP aeroservoelasticity studies
    • NASA TM-104058, NTIS N91-27127
    • Dogget, R. V., "NASP Aeroservoelasticity Studies," NASA TM-104058, NTIS N91-27127, 1991.
    • (1991)
    • Dogget, R.V.1
  • 189
    • 0346294142 scopus 로고
    • Structural dynamic and aeroelastic considerations for hypersonic vehicles
    • AIAA Paper 91-1255, April
    • Cazier, F. W., Jr., Ricketts, R. H., and Dogget, R. V., Jr., "Structural Dynamic and Aeroelastic Considerations for Hypersonic Vehicles," AIAA Paper 91-1255, April 1991.
    • (1991)
    • Cazier Jr., F.W.1    Ricketts, R.H.2    Dogget Jr., R.V.3
  • 191
    • 84991063705 scopus 로고
    • Multidisciplinary aeroelastic analysis of a generic hypersonic vehicle
    • NASA TM 4544, NTIS N94-27868
    • Gupta, K. K., and Peterson, K. L., "Multidisciplinary Aeroelastic Analysis of a Generic Hypersonic Vehicle," NASA TM 4544, NTIS N94-27868, 1993.
    • (1993)
    • Gupta, K.K.1    Peterson, K.L.2
  • 196
    • 0027628154 scopus 로고
    • Active control of aerothermoelastic effects for a conceptual hypersonic aircraft
    • Heeg, J., and Gilbert, M. G., "Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft," Journal of Aircraft, Vol. 30, 1993, pp. 453-458.
    • (1993) Journal of Aircraft , vol.30 , pp. 453-458
    • Heeg, J.1    Gilbert, M.G.2
  • 197
    • 0029275787 scopus 로고
    • Impact of aeroelastic-propulsive interactions on flight dynamics of hypersonic vehicles
    • Raney, D. L., McMinn, J. D., and Pototzky, A. S., "Impact of Aeroelastic-Propulsive Interactions on Flight Dynamics of Hypersonic Vehicles," Journal of Aircraft, Vol. 32, No. 2, 1995, pp. 355-362.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 355-362
    • Raney, D.L.1    Mcminn, J.D.2    Pototzky, A.S.3
  • 198
    • 0029276935 scopus 로고
    • CFD-based aerodynamic approximation concepts optimization of a two-dimensional scramjet vehicle
    • McQuade, P. D., Eberhardt, S., and Livne, E., "CFD-Based Aerodynamic Approximation Concepts Optimization of a Two-Dimensional Scramjet Vehicle," Journal of Aircraft, Vol. 32, No. 2, 1995, pp. 262-269.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 262-269
    • Mcquade, P.D.1    Eberhardt, S.2    Livne, E.3
  • 199
    • 0041475864 scopus 로고    scopus 로고
    • Modeling approaches to hypersonic aerothermoelasticity with application to reusable launch vehicles
    • AIAA Paper 2003-1967, April
    • Thuruthimattam, B. J., Friedmann, P. P., McNamara, J. J., and Powell, K. G., "Modeling Approaches to Hypersonic Aerothermoelasticity with Application to Reusable Launch Vehicles," AIAA Paper 2003-1967, April 2003.
    • (2003)
    • Thuruthimattam, B.J.1    Friedmann, P.P.2    Mcnamara, J.J.3    Powell, K.G.4
  • 202
    • 0041287333 scopus 로고    scopus 로고
    • Review of nonlinear panel flutter at supersonic and hypersonic speeds
    • Mei, C., Abdel-Motagly, K., and Chen, R., "Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds," Applied Mechanics Reviews, 1998.
    • (1998) Applied Mechanics Reviews
    • Mei, C.1    Abdel-Motagly, K.2    Chen, R.3
  • 204
    • 24544471764 scopus 로고    scopus 로고
    • Process and device for damping vibrations or preventing their appearance in aircraft airframes in transonic flight
    • U.S. Patent 5,890,675, 6 April
    • Lacabanne, M., and Martinage, T., "Process and Device for Damping Vibrations or Preventing Their Appearance in Aircraft Airframes in Transonic Flight," U.S. Patent 5,890,675, 6 April 1999.
    • (1999)
    • Lacabanne, M.1    Martinage, T.2
  • 205
    • 24544432236 scopus 로고
    • Apparatus and methods for reducing aircraft lifting surface flutter
    • U.S. Patent 5,054,715, 8 Oct.
    • Hager, T. R., Lakin, G. C., and Rogers, J. T., "Apparatus and Methods for Reducing Aircraft Lifting Surface Flutter," U.S. Patent 5,054,715, 8 Oct. 1991.
    • (1991)
    • Hager, T.R.1    Lakin, G.C.2    Rogers, J.T.3
  • 206
    • 85003395055 scopus 로고
    • Wing the stores flutter on variable sweep wing aircraft
    • AGARD CP-162, April
    • Sensburg, O., Lotze, A., and Haidl, G., "Wing the Stores Flutter on Variable Sweep Wing Aircraft," AGARD CP-162, April 1975.
    • (1975)
    • Sensburg, O.1    Lotze, A.2    Haidl, G.3
  • 207
    • 0042007454 scopus 로고
    • Asymmetric store flutter
    • AGARD R-668, Consideration Wing/Stores Flutter
    • Lotze, A., "Asymmetric Store Flutter," AGARD R-668, Consideration Wing/Stores Flutter, 1978.
    • (1978)
    • Lotze, A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.