메뉴 건너뛰기




Volumn 43, Issue 1, 2006, Pages 157-164

Induced drag reduction using aeroelastic tailoring with adaptive control surfaces

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; DEFLECTION (STRUCTURES); STIFFNESS; SURFACE PHENOMENA;

EID: 33644631494     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.12040     Document Type: Article
Times cited : (84)

References (32)
  • 1
    • 15944370416 scopus 로고    scopus 로고
    • Aeroelastic tailoring for improved UAV performance
    • April
    • Weisshaar, T. A., Nam, C. H., and Batista-Rodriguez, A., "Aeroelastic Tailoring for Improved UAV Performance," AIAA Paper 98-1757, April 1998.
    • (1998) AIAA Paper , vol.98 , Issue.1757
    • Weisshaar, T.A.1    Nam, C.H.2    Batista-Rodriguez, A.3
  • 3
    • 0022544782 scopus 로고
    • Aeroelastic tailoring-theory, practice, promise
    • Shirk, M. H., Hertz, T. J., and Weisshaar, T. A., "Aeroelastic 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
  • 6
    • 84888808301 scopus 로고
    • Static aeroelasticity in combat aircraft-secondary considerations of static aeroelastic effects on high performance aircraft
    • Rodden, W. P., "Static Aeroelasticity in Combat Aircraft-Secondary Considerations of Static Aeroelastic Effects on High Performance Aircraft, " Proceedings of the Static Aeroelasticity in Combat Aircraft, 1985, p. 42.
    • (1985) Proceedings of the Static Aeroelasticity in Combat Aircraft , pp. 42
    • Rodden, W.P.1
  • 7
    • 0004825913 scopus 로고
    • The minimum induced drag of airfoils
    • Munk, M. M., "The Minimum Induced Drag of Airfoils," NACA TR 121, 1921.
    • (1921) NACA TR , vol.121
    • Munk, M.M.1
  • 8
    • 0004120097 scopus 로고
    • Princeton Univ. Press, NJ
    • Jones, R. T., Wing Theory, Princeton Univ. Press, NJ, 1990, pp. 105-114.
    • (1990) Wing Theory , pp. 105-114
    • Jones, R.T.1
  • 9
    • 84888799751 scopus 로고
    • "Means for Controlling Aerodynamically Induced Twist," U.S. Patent 4,330,100, 18 May
    • Elber, W., "Means for Controlling Aerodynamically Induced Twist," U.S. Patent 4,330,100, 18 May 1982.
    • (1982)
    • Elber, W.1
  • 11
    • 0019584841 scopus 로고
    • Mission adaptive wing system for tactical aircraft
    • Gilbert, W. W., "Mission Adaptive Wing System for Tactical Aircraft," Journal of Aircraft, Vol. 18, No. 7, 1981, pp. 597-602.
    • (1981) Journal of Aircraft , vol.18 , Issue.7 , pp. 597-602
    • Gilbert, W.W.1
  • 12
    • 34547159381 scopus 로고
    • Composite wing for transonic improvement; Vol. I - Composite wing aeroelastic response study
    • Air Force Flight Dynamics Laboratory, Wright-Patterson AFB, OH
    • Waddoups, M. E., Smith, C. B., and McMickle., R. W., "Composite Wing for Transonic Improvement; Vol. I - Composite Wing Aeroelastic Response Study," Air Force Flight Dynamics Laboratory, AFFDL-TR-71-24, Wright-Patterson AFB, OH, 1972.
    • (1972) AFFDL-TR-71-24
    • Waddoups, M.E.1    Smith, C.B.2    McMickle, R.W.3
  • 14
    • 84896878145 scopus 로고
    • Wind tunnel test of an improved computer-controlled variable-geometry wing (self-optimizing flexible technology wing program)
    • Arnold Engineering Development Center
    • Levinsky, E. S., et al., "Wind Tunnel Test of an Improved Computer-Controlled Variable-Geometry Wing (Self-Optimizing Flexible Technology Wing Program)," Arnold Engineering Development Center, AEDC-TR-80-42, 1981.
    • (1981) AEDC-TR-80-42
    • Levinsky, E.S.1
  • 15
    • 84915226631 scopus 로고
    • Mission adaptive wing camber control systems for transport aircraft
    • Oct.
    • Renken, J. H., "Mission Adaptive Wing Camber Control Systems for Transport Aircraft," AIAA Paper 85-5006, Oct. 1985.
    • (1985) AIAA Paper , vol.85 , Issue.5006
    • Renken, J.H.1
  • 16
    • 0003829422 scopus 로고
    • Executive summary AFTI/F-111 mission adaptive wing
    • Flight Dynamics Lab., Wright-Patterson AFB, OH, Sept.
    • Hall, J. M., "Executive Summary AFTI/F-111 Mission Adaptive Wing," Flight Dynamics Lab., WRDC-TR-89-3083, Wright-Patterson AFB, OH, Sept. 1989.
    • (1989) WRDC-TR-89-3083
    • Hall, J.M.1
  • 17
    • 33644615217 scopus 로고    scopus 로고
    • Development of a real-time transport performance optimization methodology
    • Jan.
    • Gilyard, G., "Development of a Real-Time Transport Performance Optimization Methodology," AIAA Paper 96-0093, Jan. 1996.
    • (1996) AIAA Paper , vol.96 , Issue.93
    • Gilyard, G.1
  • 18
    • 38249014992 scopus 로고
    • Adaptive aeroelastic composite wings - Control and optimization issues
    • Weisshaar, T. A., and Ehlers, S. M., "Adaptive Aeroelastic Composite Wings - Control and Optimization Issues," Composites Engineering, Vol. 2, No. 5-7, 1992, pp. 457-476.
    • (1992) Composites Engineering , vol.2 , Issue.5-7 , pp. 457-476
    • Weisshaar, T.A.1    Ehlers, S.M.2
  • 19
    • 33644624073 scopus 로고
    • Maximizing deflections produced by induced strain beam-like actuators for transonic drag reduction
    • AIAA, Washington, DC
    • Muller, M. B., and Weisshaar, T. A., "Maximizing Deflections Produced by Induced Strain Beam-Like Actuators for Transonic Drag Reduction," Proceedings of the AIAA/ASME Adaptive Structures Forum, AIAA, Washington, DC, 1994, pp. 388-401.
    • (1994) Proceedings of the AIAA/ASME Adaptive Structures Forum , pp. 388-401
    • Muller, M.B.1    Weisshaar, T.A.2
  • 20
    • 0003715026 scopus 로고
    • Active Flexible Wing (AFW) technology
    • Wright Aeronautical Lab., Wright-Patterson AFB, OH
    • Miller, G., "Active Flexible Wing (AFW) Technology," Wright Aeronautical Lab., AFWAL-TR-87-3096, Wright-Patterson AFB, OH, 1988.
    • (1988) AFWAL-TR-87-3096
    • Miller, G.1
  • 21
    • 0026869470 scopus 로고
    • Application of AFW technology to the agile falcon
    • Pendleton, E. E., Lee, M., and Wasserman, L., "Application of AFW 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
    • Pendleton, E.E.1    Lee, M.2    Wasserman, L.3
  • 23
    • 0029219120 scopus 로고
    • A summary of the AFW program
    • Perry, B., Cole, S., and Miller, G., "A Summary of the AFW Program," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 10-15.
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 10-15
    • Perry, B.1    Cole, S.2    Miller, G.3
  • 26
    • 84896836173 scopus 로고    scopus 로고
    • Development of preliminary design models for active aeroelastic wing application
    • Air Force Wright Laboratory
    • Eastep, F. E., "Development of Preliminary Design Models for Active Aeroelastic Wing Application," Air Force Wright Laboratory, AFWL-TR-97-3019, 1997.
    • (1997) AFWL-TR-97-3019
    • Eastep, F.E.1
  • 28
    • 84888772421 scopus 로고
    • "Active Flexible Wing Aircraft Control System," U.S. Patent 5,082,207, 21 Jan.
    • Tulinius, J., "Active Flexible Wing Aircraft Control System," U.S. Patent 5,082,207, 21 Jan. 1992.
    • (1992)
    • Tulinius, J.1
  • 29
    • 33644617733 scopus 로고
    • Forward swept wing static aeroelasticity
    • Air Force Flight Dynamics Lab., Wright-Patterson AFB, OH, June
    • Weisshaar, T. A., "Forward Swept Wing Static Aeroelasticity," Air Force Flight Dynamics Lab., AFFDL-TR-79-3087, Wright-Patterson AFB, OH, June 1979.
    • (1979) AFFDL-TR-79-3087
    • Weisshaar, T.A.1
  • 30
    • 85001895100 scopus 로고
    • A method for calculating the subsonic steady-state loading on an airplane with a wing of arbitrary plan form and stiffness
    • Gray, W., and Schenk, K., "A Method for Calculating the Subsonic Steady-State Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness," NACA-TN-3030, July 1953.
    • (1953) NACA-TN-3030, July
    • Gray, W.1    Schenk, K.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.