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Volumn 42, Issue 6, 2005, Pages 1589-1596

Limit-cycle oscillation flight-test results for asymmetric store configurations

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT MODELS; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS;

EID: 29544441227     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (4)

References (12)
  • 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
    • 0001106389 scopus 로고
    • Semi-empirical unsteady aerodynamics for modeling aircraft limit cycle oscillations and other non-linear aeroelastic problems
    • Royal Aeronautical Society, London
    • 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, Vol. 2, Royal Aeronautical Society, London, 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
  • 3
    • 16244376242 scopus 로고
    • A semi-empirical unsteady nonlinear aerodynamic model to predict transonic LCO characteristics of fighter aircraft
    • April
    • Meijer, J. J., and Cunningham, A. M., Jr., "A Semi-Empirical Unsteady Nonlinear Aerodynamic Model to Predict Transonic LCO Characteristics of Fighter Aircraft," AIAA Paper 95-1340, April 1995.
    • (1995) AIAA Paper , vol.95 , Issue.1340
    • Meijer, J.J.1    Cunningham Jr., A.M.2
  • 4
    • 0031678210 scopus 로고    scopus 로고
    • Limit-cycle oscillation studies of a fighter with external stores
    • April
    • Chen, P. C., Sarhaddi, D., and Liu, D. D., "Limit-Cycle Oscillation Studies of a Fighter with External Stores," AIAA Paper 98-1727, April 1998.
    • (1998) AIAA Paper , vol.98 , Issue.1727
    • Chen, P.C.1    Sarhaddi, D.2    Liu, D.D.3
  • 5
    • 0034272640 scopus 로고    scopus 로고
    • Limit cycle oscillation flight test results of a figher with external stores
    • Denegri, C. M., Jr., "Limit Cycle Oscillation Flight Test Results of a Figher 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
  • 6
    • 29544443641 scopus 로고
    • Flutter of aircraft with external stores
    • McDonnell Aircraft Co., St. Louis, MO
    • Katz, H., "Flutter of Aircraft with External Stores," U.S. Air Force Aircraft/Stores Compatibility Symposium, McDonnell Aircraft Co., St. Louis, MO, 1969, pp. 1-15.
    • (1969) U.S. Air Force Aircraft/Stores Compatibility Symposium , pp. 1-15
    • Katz, H.1
  • 7
    • 85069350477 scopus 로고
    • Wing with stores flutter on variable sweep wing aircraft
    • NATO, Neuilly Sur Seine, France
    • Sensburg, O., Lotze, A., and Haidl, G., "Wing with Stores Flutter on Variable Sweep Wing Aircraft," AGARD Conference Proceedings, No. 162, NATO, Neuilly Sur Seine, France, 1974, pp. 6.1-6.19.
    • (1974) AGARD Conference Proceedings , Issue.162
    • Sensburg, O.1    Lotze, A.2    Haidl, G.3
  • 8
    • 0017791884 scopus 로고
    • Asymmetric store flutter
    • NATO, Neuilly Sur Seine, France, April
    • Lotze, A., "Asymmetric Store Flutter," AGARD, Rept. 668, NATO, Neuilly Sur Seine, France, April 1978, pp. 1-20.
    • (1978) AGARD, Rept. , vol.668 , pp. 1-20
    • Lotze, A.1
  • 9
    • 0018525936 scopus 로고
    • Calculation of critical flutter speeds of an aircraft in subsonic flow
    • Oct.
    • Maricic, N. L., "Calculation of Critical Flutter Speeds of an Aircraft in Subsonic Flow," Computers and Structures, Vol. 12, Oct. 1980, pp. 475-482.
    • (1980) Computers and Structures , vol.12 , pp. 475-482
    • Maricic, N.L.1
  • 10
    • 29544452454 scopus 로고
    • Effects of symmetric and asymmetric modes on transonic aeroelastic characteristics of full-span wing-body configurations
    • April
    • Guruswamy, G. P., and Tu, E. L., "Effects of Symmetric and Asymmetric Modes on Transonic Aeroelastic Characteristics of Full-Span Wing-Body Configurations," AIAA Paper 88-2308, April 1988.
    • (1988) AIAA Paper , vol.88 , Issue.2308
    • Guruswamy, G.P.1    Tu, E.L.2
  • 11
    • 84964311108 scopus 로고    scopus 로고
    • F-16 limit cycle oscillation testing with asymmetric stores
    • June
    • Dawson, K. S., and Sussingham, J. C., "F-16 Limit Cycle Oscillation Testing with Asymmetric Stores," AIAA Paper 99-3142, June 1999.
    • (1999) AIAA Paper , vol.99 , Issue.3142
    • Dawson, K.S.1    Sussingham, J.C.2
  • 12
    • 85087252662 scopus 로고
    • F-16 flutter testing at Eglin Air Force Base
    • April
    • Dreyer, C. A., and Shoch, D. L., "F-16 Flutter Testing at Eglin Air Force Base," AIAA Paper 86-9819, April 1986.
    • (1986) AIAA Paper , vol.86 , Issue.9819
    • Dreyer, C.A.1    Shoch, D.L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.