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Volumn , Issue , 2002, Pages

Control of F/A-18 vertical tail buffet by vortical blowing

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; BOMBERS; BUFFETING; FLUID STRUCTURE INTERACTION; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT; VERTICAL STABILIZERS; VORTEX FLOW;

EID: 85088344008     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-948     Document Type: Conference Paper
Times cited : (5)

References (20)
  • 10
    • 0028497486 scopus 로고
    • Vortical Flow Structure near the F/A-18 LEX at High Incidence
    • Lee, B. and Valerio, N., "Vortical Flow Structure near the F/A-18 LEX at High Incidence, " Journal of Aircraft, Vol. 31, No. 5, 1994, pp. 1221-1223.
    • (1994) Journal of Aircraft , vol.31 , Issue.5 , pp. 1221-1223
    • Lee, B.1    Valerio, N.2
  • 11
    • 0027591873 scopus 로고
    • Effects of Blowing on Delta Wing Vortices During Dynamic Pitching
    • May
    • Miller, L. S. and Gile, B. E., "Effects of Blowing on Delta Wing Vortices During Dynamic Pitching, " Journal of Aircraft, Vol. 30, May 1993, pp. 334-339.
    • (1993) Journal of Aircraft , vol.30 , pp. 334-339
    • Miller, L.S.1    Gile, B.E.2
  • 12
    • 0019246616 scopus 로고
    • Effects of Span wise Blowing on Two Fighter Airplane Configurations
    • Dec
    • Anglin, E. L. and Satran, D., "Effects of Span wise Blowing on Two Fighter Airplane Configurations, " Journal of Aircraft, Vol. 17, Dec. 1980, pp. 883-889.
    • (1980) Journal of Aircraft , vol.17 , pp. 883-889
    • Anglin, E.L.1    Satran, D.2
  • 13
    • 0023060875 scopus 로고
    • Performance Augmentation of a 60-Degree Delta Aircraft Configuration by Spanwise Blowing
    • Nov
    • Seginer, A. and Salomon, M., "Performance Augmentation of a 60-Degree Delta Aircraft Configuration by Spanwise Blowing, " Journal of Aircraft, Vol. 23, Nov. 1986, pp. 801-807.
    • (1986) Journal of Aircraft , vol.23 , pp. 801-807
    • Seginer, A.1    Salomon, M.2
  • 14
    • 85085402482 scopus 로고    scopus 로고
    • Control of Twin-Tail Buffet Responses using Normal Leading-Edge Blowing
    • AIAA 2000-4227, Denver, CO, August 14-17
    • Sheta, E. F., "Control of Twin-Tail Buffet Responses using Normal Leading-Edge Blowing, " AIAA 2000-4227, 18th AIAA Applied Aerodynamic Conference, Denver, CO, August 14-17, 2000.
    • (2000) 18th AIAA Applied Aerodynamic Conference
    • Sheta, E.F.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.