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Volumn , Issue , 2000, Pages

Effect of stream-wise fences on twin-tail buffet responses

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ASPECT RATIO; FENCES; FLEXIBLE WINGS; SUPERSONIC AIRCRAFT; SWEPT WINGS;

EID: 85087605852     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4410     Document Type: Conference Paper
Times cited : (3)

References (18)
  • 5
    • 0003861880 scopus 로고
    • Experimental Investigation of Vortex-Fin Interaction
    • AIAA 93-0050, Reno, NV
    • Washburn, A. E., Jenkins, L. N. and Ferman, M. A., Experimental Investigation of Vortex-Fin Interaction, AIAA 93-0050, AIAA 31st ASM, Reno, NV, 1993.
    • (1993) AIAA 31st ASM
    • Washburn, A.E.1    Jenkins, L.N.2    Ferman, M.A.3
  • 7
    • 0009647817 scopus 로고    scopus 로고
    • Effect of Dynamic Rolling Oscillations on Twin-Tail Buffet Response
    • AIAA 99-0792, Reno, NV
    • Sheta, E. F. and Kandii, O. A., Effect of Dynamic Rolling Oscillations on Twin-Tail Buffet Response, AIAA 99-0792, AIAA 37th ASM, Reno, NV, 1999.
    • (1999) AIAA 37th ASM
    • Sheta, E.F.1    Kandii, O.A.2
  • 8
    • 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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.