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Volumn , Issue , 2003, Pages

In-flight wing deformation characteristics during limit cycle oscillations

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC MODES; DEFORMATION CHARACTERISTICS; FLIGHT CONDITIONS; FLUTTER ANALYSIS; IN-FLIGHT WING DEFORMATION; LIMIT CYCLE OSCILLATION (LCO); MISSILE LAUNCHER; WING DEFORMATION;

EID: 84896855655     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (17)
  • 1
    • 0034273920 scopus 로고    scopus 로고
    • Limit Cycle Oscillation Characteristics of Fighter Aircraft
    • Bunton, R. W., and Denegri, C. M., Jr., "Limit Cycle Oscillation Characteristics of Fighter Aircraft, " Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 916-918.
    • (2000) Journal of Aircraft , vol.37 , Issue.5 , pp. 916-918
    • Bunton, R.W.1    Denegri Jr., C.M.2
  • 2
    • 0003261503 scopus 로고
    • Limit Cycle Oscillation and Flight Flutter Testing
    • Society of Flight Test Engineers, Lancaster, CA, 3. 4-1 to 3. 4-12
    • st Annual Symposium Proceedings, Society of Flight Test Engineers, Lancaster, CA, 1990, pp. 3. 4-1 to 3. 4-12.
    • (1990) st Annual Symposium Proceedings
    • Norton, W.J.1
  • 3
    • 0001106389 scopus 로고
    • Semi-Empirical Unsteady Aerodynamics for Modeling Aircraft Limit Cycle Oscillations and Other Non-Linear Aeroelastic Problems
    • Royal Aeronautical Society, London, 74. 1-74. 14
    • Cunningham, A. M., Jr., and Meijer, J. J., "Semi-Empirical Unsteady Aerodynamics for Modeling Aircraft Limit Cycle Oscillations and Other Non-Linear Aeroelastic Problems, " Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, Royal Aeronautical Society, London, Vol. 2, 1995, pp. 74. 1-74. 14.
    • (1995) Proceedings of the International Forum on Aeroelasticity and Structural Dynamics , vol.2
    • Cunningham Jr., A.M.1    Meijer, J.J.2
  • 6
    • 0035441062 scopus 로고    scopus 로고
    • Limit Cycle Oscillation Prediction Using Artificial Neural Networks
    • Denegri, C. M., Jr., and Johnson, M. R., "Limit Cycle Oscillation Prediction Using Artificial Neural Networks, " Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 887-895.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.5 , pp. 887-895
    • Denegri Jr., C.M.1    Johnson, M.R.2
  • 7
    • 0037226451 scopus 로고    scopus 로고
    • Comparison of Static and Dynamic Neural Networks for Limit Cycle Oscillation Prediction
    • Johnson, M. R., and Denegri, C. M., Jr., "Comparison of Static and Dynamic Neural Networks for Limit Cycle Oscillation Prediction, " Journal of Aircraft, Vol. 40, No. 1, 2003, pp. 194-203.
    • (2003) Journal of Aircraft , vol.40 , Issue.1 , pp. 194-203
    • Johnson, M.R.1    Denegri Jr, C.M.2
  • 13
    • 0034272640 scopus 로고    scopus 로고
    • Limit Cycle Oscillation Flight Test Results of a Fighter With External Stores
    • Denegri, C. M., Jr., "Limit Cycle Oscillation Flight Test Results of a Fighter With External Stores, " Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 761-769.
    • (2000) Journal of Aircraft , vol.37 , Issue.5 , pp. 761-769
    • Denegri Jr., C.M.1
  • 15
    • 85007685430 scopus 로고
    • A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows
    • February
    • Albano, E., and Rodden, W. P., "A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows, " AIAA Journal, Vol. 7, No. 2, February 1969, pp. 279-285.
    • (1969) AIAA Journal , vol.7 , Issue.2 , pp. 279-285
    • Albano, E.1    Rodden, W.P.2
  • 16
    • 0015291061 scopus 로고
    • Interpolation Using Surface Splines
    • February
    • Harder, R. L., and Desmarais, R. N., "Interpolation Using Surface Splines, " Journal of Aircraft, Vol. 9, No. 2, February 1972, pp. 189-191.
    • (1972) Journal of Aircraft , vol.9 , Issue.2 , pp. 189-191
    • Harder, R.L.1    Desmarais, R.N.2
  • 17
    • 0034833242 scopus 로고    scopus 로고
    • Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing
    • Tang, D. and Dowell, E. H., "Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing, " AIAA Journal, Vol. 39, No. 1, 2001, pp. 15-19.
    • (2001) AIAA Journal , vol.39 , Issue.1 , pp. 15-19
    • Tang, D.1    Dowell, E.H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.