메뉴 건너뛰기




Volumn 40, Issue 2, 2003, Pages 162-173

Aeroelasticity of composite aerovehicle wings in supersonic flows

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; ANISOTROPY; STRAIN; SUPERSONIC AERODYNAMICS; SUPERSONIC FLOW;

EID: 0037362462     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3950     Document Type: Article
Times cited : (19)

References (36)
  • 1
    • 0022544782 scopus 로고
    • Aeroelastic tailoring-theory, practice and promise
    • Shirk, M. H., Hertz, T. J., and Weisshaar, T. A., "Aeroelastic Tailoring-Theory, Practice and 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
  • 2
    • 38249013753 scopus 로고
    • On the static aeroelastic tailoring of composite aircraft swept wings modeled as thin-walled beam structures
    • Librescu, L., and Song, O., "On the Static Aeroelastic Tailoring of Composite Aircraft Swept Wings Modeled as Thin-Walled Beam Structures," Composites Engineering, Vol. 2, No. 5-7, 1992, pp. 497-512.
    • (1992) Composites Engineering , vol.2 , Issue.5-7 , pp. 497-512
    • Librescu, L.1    Song, O.2
  • 5
    • 0026188364 scopus 로고
    • Formulation and evaluation of an analytical model for composite box-beams
    • Smith, E. C., and Chopra, I., "Formulation and Evaluation of an Analytical Model for Composite Box-Beams," Journal of American Helicopter Society, Vol. 36, No. 3, 1991, pp. 23-35.
    • (1991) Journal of American Helicopter Society , vol.36 , Issue.3 , pp. 23-35
    • Smith, E.C.1    Chopra, I.2
  • 7
    • 85024597309 scopus 로고
    • Behavior of thin-walled beams made of advanced composite materials and incorporating non-classical effects
    • Librescu, L., and Song, O., "Behavior of Thin-Walled Beams Made of Advanced Composite Materials and Incorporating Non-Classical Effects," Applied Mechanics Reviews, Vol. 44, No. 11, Pt. 2, 1991, pp. S174-S180.
    • (1991) Applied Mechanics Reviews , vol.44 , Issue.11 PART 2
    • Librescu, L.1    Song, O.2
  • 8
    • 0027912271 scopus 로고
    • Free vibration of anisotropic composite thin-walled beams of closed cross-section contour
    • Song, O., and Librescu, L., "Free Vibration of Anisotropic Composite Thin-Walled Beams of Closed Cross-Section Contour," Journal of Sound and Vibration, Vol. 167, No. 1, 1993, pp. 129-147.
    • (1993) Journal of Sound and Vibration , vol.167 , Issue.1 , pp. 129-147
    • Song, O.1    Librescu, L.2
  • 10
    • 0031271017 scopus 로고    scopus 로고
    • Thick-walled composite beam theory including 3-D elastic effects and torsional warping
    • Kim, C., and White, S. R., "Thick-Walled Composite Beam Theory Including 3-D Elastic Effects and Torsional Warping," International Journal of Solids and Structures, Vol. 34, No. 31-32, 1997, pp. 4237-4259.
    • (1997) International Journal of Solids and Structures , vol.34 , Issue.31-32 , pp. 4237-4259
    • Kim, C.1    White, S.R.2
  • 11
    • 0000243867 scopus 로고
    • A geometrically non-linear theory for laminated anisotropic thin-walled beams
    • Bhaskar, K., and Librescu, L., "A Geometrically Non-Linear Theory for Laminated Anisotropic Thin-Walled Beams," International Journal of Engineering Science, Vol. 33, No. 9. 1995, pp. 1331-1344.
    • (1995) International Journal of Engineering Science , vol.33 , Issue.9 , pp. 1331-1344
    • Bhaskar, K.1    Librescu, L.2
  • 12
    • 0030247698 scopus 로고    scopus 로고
    • Higher-order shear deformation theory for thin-walled composite beams
    • Suresh, J. K., and Nagaraj, V. T., "Higher-Order Shear Deformation Theory for Thin-Walled Composite Beams," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 978-986.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 978-986
    • Suresh, J.K.1    Nagaraj, V.T.2
  • 13
    • 0026157277 scopus 로고
    • Vibration analysis of laminated composite thin-walled beams using finite elements
    • Wu, X. X., and Sun, C. T., "Vibration Analysis of Laminated Composite Thin-Walled Beams Using Finite Elements," AIAA Journal, Vol. 29, No. 5, 1991, pp. 736-742.
    • (1991) AIAA Journal , vol.29 , Issue.5 , pp. 736-742
    • Wu, X.X.1    Sun, C.T.2
  • 14
    • 0000202690 scopus 로고
    • Theory of anisotropic thin-walled closed cross-section beams
    • Berdichevski, V. L., Armanios, E., and Badir, A., "Theory of Anisotropic Thin-Walled Closed Cross-Section Beams," Composite Engineering, Vol. 2, No. 5-7, 1992, pp. 411-432.
    • (1992) Composite Engineering , vol.2 , Issue.5-7 , pp. 411-432
    • Berdichevski, V.L.1    Armanios, E.2    Badir, A.3
  • 15
    • 0001644704 scopus 로고
    • Structural response of composite beams and blades with elastic couplings
    • Chandra, R., and Chopra, I., "Structural Response of Composite Beams and Blades with Elastic Couplings," Composites Engineering, Vol. 2, No. 5-7, 1992, pp. 347-374.
    • (1992) Composites Engineering , vol.2 , Issue.5-7 , pp. 347-374
    • Chandra, R.1    Chopra, I.2
  • 16
    • 0001215010 scopus 로고    scopus 로고
    • Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings
    • Karpouzion, G., and Librescu, L., "Nonclassical Effects on Divergence and Flutter of Anisotropic Swept Aircraft Wings," AIAA Journal, Vol. 34, No. 4, 1996, pp. 786-794.
    • (1996) AIAA Journal , vol.34 , Issue.4 , pp. 786-794
    • Karpouzion, G.1    Librescu, L.2
  • 17
    • 0036624127 scopus 로고    scopus 로고
    • On a shear-deformable theory of anisotropic thin-walled beams: Further contribution and validation
    • Qin, Z., and Librescu, L., "On a Shear-Deformable Theory of Anisotropic Thin-Walled Beams: Further Contribution and Validation," Journal of Composite Structures, Vol. 56, No. 4, 2002, pp. 345-358.
    • (2002) Journal of Composite Structures , vol.56 , Issue.4 , pp. 345-358
    • Qin, Z.1    Librescu, L.2
  • 19
    • 0031189057 scopus 로고    scopus 로고
    • Direct calculation of three-dimensional indicial lift response using computational fluid dynamics
    • Singh, R., and Baeder, J. D., "Direct Calculation of Three-Dimensional Indicial Lift Response Using Computational Fluid Dynamics," Journal of Aircraft, Vol. 34, No. 4, 1997, pp. 465-471.
    • (1997) Journal of Aircraft , vol.34 , Issue.4 , pp. 465-471
    • Singh, R.1    Baeder, J.D.2
  • 20
    • 0027593903 scopus 로고
    • Indicial lift approximations for two-dimensional subsonic flow as obtained from oscillatory measurements
    • Leishman, J., "Indicial Lift Approximations for Two-Dimensional Subsonic Flow as Obtained from Oscillatory Measurements," Journal of Aircraft, Vol. 30, No. 3. 1993, pp. 340-351.
    • (1993) Journal of Aircraft , vol.30 , Issue.3 , pp. 340-351
    • Leishman, J.1
  • 21
    • 0036086175 scopus 로고    scopus 로고
    • Aeroelastic response of a 2-D airfoil in a compressible flow field and exposed to blast loading
    • Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Airfoil in a Compressible Flow Field and Exposed to Blast Loading," Aerospace Science and Technology, Vol. 6, No. 4, 2002, pp. 259-272.
    • (2002) Aerospace Science and Technology , vol.6 , Issue.4 , pp. 259-272
    • Marzocca, P.1    Librescu, L.2    Chiocchia, G.3
  • 22
    • 0024088694 scopus 로고
    • Validation of approximate indicial aerodynamic functions for two-dimensional subsonic flow
    • Leishman, J. G., "Validation of Approximate Indicial Aerodynamic Functions for Two-Dimensional Subsonic Flow," Journal of Aircraft, Vol. 25, No. 10, 1988, pp. 914-922.
    • (1988) Journal of Aircraft , vol.25 , Issue.10 , pp. 914-922
    • Leishman, J.G.1
  • 23
    • 0027664172 scopus 로고
    • Application of nonlinear systems theory to transonic unsteady aerodynamic responses
    • Silva, W. A., "Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses," Journal of Aircraft, Vol. 30, No. 5, 1993, pp. 660-668.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 660-668
    • Silva, W.A.1
  • 25
    • 0036263410 scopus 로고    scopus 로고
    • Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds
    • Qin, Z., Marzocca, P., and Librescu, L., "Aeroelastic Instability and Response of Advanced Aircraft Wings at Subsonic Flight Speeds," Aerospace Science and Technology, Vol. 6, No. 3, 2002, pp. 195-208.
    • (2002) Aerospace Science and Technology , vol.6 , Issue.3 , pp. 195-208
    • Qin, Z.1    Marzocca, P.2    Librescu, L.3
  • 26
    • 0035218131 scopus 로고    scopus 로고
    • Aeroelastic response of 2-D lifting surfaces to gust and arbitrary explosive loading signatures
    • Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of 2-D Lifting Surfaces to Gust and Arbitrary Explosive Loading Signatures," International Journal of Impact Engineering, Vol. 25, No. 1, 2001, pp. 41-65.
    • (2001) International Journal of Impact Engineering , vol.25 , Issue.1 , pp. 41-65
    • Marzocca, P.1    Librescu, L.2    Chiocchia, G.3
  • 27
    • 0031621506 scopus 로고    scopus 로고
    • Dynamic response of cantilevered thin-walled beams to blast and sonic-boom loadings
    • Librescu, L., and Na, S. S., "Dynamic Response of Cantilevered Thin-Walled Beams to Blast and Sonic-Boom Loadings," Shock and Vibration, No. 5, 1998. pp. 23-33.
    • (1998) Shock and Vibration , Issue.5 , pp. 23-33
    • Librescu, L.1    Na, S.S.2
  • 29
    • 0002876346 scopus 로고    scopus 로고
    • Refined structural modeling for enhancing vibrations and aeroelastic characteristics of composite aircraft wings
    • Librescu, L., Meirovitch, L., and Song, O., "Refined Structural Modeling for Enhancing Vibrations and Aeroelastic Characteristics of Composite Aircraft Wings," La Recherche Aérospatiale, No. 1, 1996, pp. 23-35.
    • (1996) La Recherche Aérospatiale , Issue.1 , pp. 23-35
    • Librescu, L.1    Meirovitch, L.2    Song, O.3
  • 30
    • 0003894619 scopus 로고    scopus 로고
    • Ph.D. Dissertation, Dept. of Engineering Science and Mechanics, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, Oct.
    • Qin, Z., "Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams," Ph.D. Dissertation, Dept. of Engineering Science and Mechanics, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, Oct. 2001.
    • (2001) Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams
    • Qin, Z.1
  • 31
    • 0031199690 scopus 로고    scopus 로고
    • Control of cantilevers vibration via structural tailoring and adaptive materials
    • Librescu, L., Meirovitch, L., and Na, S. S., "Control of Cantilevers Vibration via Structural Tailoring and Adaptive Materials," AIAA Journal, Vol. 35, No. 8, 1997, pp. 1309-1315.
    • (1997) AIAA Journal , vol.35 , Issue.8 , pp. 1309-1315
    • Librescu, L.1    Meirovitch, L.2    Na, S.S.3
  • 32
    • 0003056887 scopus 로고
    • Vibration and buckling characteristics of composite cylindrical panels incorporating the effects of a higher order shear theory
    • Palazotto, A. N., and Linnemann, P. E., "Vibration and Buckling Characteristics of Composite Cylindrical Panels Incorporating the Effects of a Higher Order Shear Theory," International Journal of Solids and Structures, Vol. 28, No. 3. 1991, pp. 341-361.
    • (1991) International Journal of Solids and Structures , vol.28 , Issue.3 , pp. 341-361
    • Palazotto, A.N.1    Linnemann, P.E.2
  • 33
    • 0002406986 scopus 로고
    • The flutter of a uniform cantilever wing with tip weights
    • Goland, M., and Luke, Y., "The Flutter of a Uniform Cantilever Wing with Tip Weights," Journal of Applied Mechanics, Vol. 15, No. 1, 1948, pp. 13-20.
    • (1948) Journal of Applied Mechanics , vol.15 , Issue.1 , pp. 13-20
    • Goland, M.1    Luke, Y.2
  • 35
    • 0026103397 scopus 로고
    • Analytical studies on static aeroelastic behavior of forward-swept composite wing structures
    • Librescu, L., and Thangjitham, S., "Analytical Studies on Static Aeroelastic Behavior of Forward-Swept Composite Wing Structures," Journal of Aircraft, Vol. 28, No. 2, 1991, pp. 151-157.
    • (1991) Journal of Aircraft , vol.28 , Issue.2 , pp. 151-157
    • Librescu, L.1    Thangjitham, S.2
  • 36
    • 85002849893 scopus 로고
    • U.S. Air Force Wright Aeronautical Lab., Final Rept. AFWAL-TR80-3137, Wright-Patterson AFB, OH, Nov.
    • Weisshaar, T. A., "Forward Swept Wing Static Aeroelasticity," U.S. Air Force Wright Aeronautical Lab., Final Rept. AFWAL-TR80-3137, Wright-Patterson AFB, OH, Nov. 1980.
    • (1980) Forward Swept Wing Static Aeroelasticity
    • Weisshaar, T.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.