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Volumn , Issue , 1997, Pages

A case for pseudo-steady aerodynamic behaviour at high motion rates

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; INCOMPRESSIBLE FLOW; WAKES;

EID: 84982318277     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (20)
  • 1
    • 0024019050 scopus 로고
    • Airfoil Dynamic Stall at Constant Pitch Rate and High Reynolds Number
    • June
    • Lorber, P. F., and Carta, F. O., "Airfoil Dynamic Stall at Constant Pitch Rate and High Reynolds Number," Journal of Aircraft, Vol. 25, June 1988, pp. 548-556.
    • (1988) Journal of Aircraft , vol.25 , pp. 548-556
    • Lorber, P.F.1    Carta, F.O.2
  • 2
    • 0025207923 scopus 로고
    • Low-Speed Unsteady Aerodynamics of a Pitching Straked Wing at High Incidence - Part I: Test Program
    • Jan
    • den Boer, R. G., and Cunningham, A. M., "Low-Speed Unsteady Aerodynamics of a Pitching Straked Wing at High Incidence - Part I: Test Program," Journal of Aircraft, Vol. 27, Jan. 1990, pp. 23-30.
    • (1990) Journal of Aircraft , vol.27 , pp. 23-30
    • Den Boer, R.G.1    Cunningham, A.M.2
  • 3
    • 0025208932 scopus 로고
    • Low-Speed Unsteady Aerodynamics of a Pitching Straked Wing at High Incidence - Part II: Harmonic Analysis
    • Jan
    • Cunningham, A. M., and den Boer, R. G., "Low-Speed Unsteady Aerodynamics of a Pitching Straked Wing at High Incidence - Part II: Harmonic Analysis," Journal of Aircraft, Vol. 27, Jan. 1990, pp. 31-41.
    • (1990) Journal of Aircraft , vol.27 , pp. 31-41
    • Cunningham, A.M.1    Den Boer, R.G.2
  • 4
    • 0019046112 scopus 로고
    • Future Fighter Technologies
    • Aug
    • Herbst, W. B., "Future Fighter Technologies," Journal of Aircraft, Vol. 17, Aug. 1980, pp. 561-566.
    • (1980) Journal of Aircraft , vol.17 , pp. 561-566
    • Herbst, W.B.1
  • 5
    • 0020782413 scopus 로고
    • Dynamics of Air Combat
    • July
    • Herbst, W. B., "Dynamics of Air Combat," Journal of Aircraft, Vol. 20, July 1983, pp. 594-598.
    • (1983) Journal of Aircraft , vol.20 , pp. 594-598
    • Herbst, W.B.1
  • 6
    • 0020294670 scopus 로고
    • Flight Control Synthesis Using Robust Observers
    • San Diego, CA, Aug
    • Rynaski, E. G., "Flight Control Synthesis Using Robust Observers," Proc. AIAA Guidance and Control Conference, San Diego, CA, Aug. 1982, pp. 825-831.
    • (1982) Proc. AIAA Guidance and Control Conference , pp. 825-831
    • Rynaski, E.G.1
  • 8
    • 0017439068 scopus 로고
    • Optimal Digital Flight Control for Advanced Fighter Aircraft
    • Jan
    • Gran, R., Berman, H., Rossi, M., "Optimal Digital Flight Control for Advanced Fighter Aircraft," Journal of Aircraft, Vol. 14, Jan. 1977, pp. 32-37.
    • (1977) Journal of Aircraft , vol.14 , pp. 32-37
    • Gran, R.1    Berman, H.2    Rossi, M.3
  • 11
    • 0030247997 scopus 로고    scopus 로고
    • Experimental Measurements of Dynamic Control Surface Effectiveness
    • Sep
    • Rennie, R. M., and Jumper, E. J., "Experimental Measurements of Dynamic Control Surface Effectiveness," Journal of Aircraft, Vol. 33, № 5, Sep. 1996, pp. 880-887.
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 880-887
    • Rennie, R.M.1    Jumper, E.J.2
  • 15
    • 0028393040 scopus 로고
    • Unsteady Lift of a Flapped Airfoil by Indicia! Concepts
    • March
    • Leishman, J. G., "Unsteady Lift of a Flapped Airfoil by Indicia! Concepts," Journal of Aircraft, Vol. 31, March 1994, pp. 288-297.
    • (1994) Journal of Aircraft , vol.31 , pp. 288-297
    • Leishman, J.G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.