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Volumn , Issue , 2003, Pages

Applying vortex breakdown empiricisms to predict aerodynamic characteristics in symmetric & asymmetric situations

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; MILITARY APPLICATIONS; REYNOLDS NUMBER; SWEPT WINGS;

EID: 85067319919     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3945     Document Type: Conference Paper
Times cited : (6)

References (20)
  • 6
    • 84897696833 scopus 로고    scopus 로고
    • Wings using Panel Methods, Attained Thrust & Euler Codes, ICAS-92
    • NANGIA, R.K., The Design of Manoeuvrable Wings using Panel Methods, Attained Thrust & Euler Codes, ICAS-92.
    • The Design of Manoeuvrable
    • Nangia, R.K.1
  • 7
    • 84897676305 scopus 로고
    • Studies of LE Thrust Phenomena
    • CARLSON, H. W. & MACK, R.J., "Studies of LE Thrust Phenomena", AIAA jo. Of Air., Vol. 17, No.12, pp. 890-7, December 1990.
    • (1990) AIAA Jo. of Air , vol.17 , Issue.12 , pp. 890-897
    • Carlson, H.W.1    Mack, R.J.2
  • 8
    • 0015039667 scopus 로고
    • Predictions of Vortex-Lift Characteristics by a LE Suction Analogy
    • POLHAMUS, E.C., "Predictions of Vortex-Lift Characteristics by a LE Suction Analogy", AIAA Jl. of Air., Vol.8, No. 4, pp.193-9, April 1971.
    • (1971) AIAA Jl. of Air , vol.8 , Issue.4 , pp. 193-199
    • Polhamus, E.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.