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Volumn 46, Issue 4, 2009, Pages 1454-1457

Aerodynamic characteristics of forward and aft swept arrow wings

Author keywords

[No Author keywords available]

Indexed keywords

FLOW VISUALIZATION; PLANFORMS; SUBSONIC AERODYNAMICS; WIND TUNNELS;

EID: 73349117145     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.43098     Document Type: Article
Times cited : (9)

References (11)
  • 1
    • 0020716855 scopus 로고
    • Wind tunnel investigation of the transonic aerodynamic characteristics of forward swept wings
    • doi:10.2514/3.44853
    • Uhuad, G. C., Weeks, T. M., and Large, R., "Wind Tunnel Investigation of the Transonic Aerodynamic Characteristics of Forward Swept Wings," Journal of Aircraft, Vol. 20, No. 3, 1983, pp. 195-202. doi:10.2514/3.44853
    • (1983) Journal of Aircraft , vol.20 , Issue.3 , pp. 195-202
    • Uhuad, G.C.1    Weeks, T.M.2    Large, R.3
  • 2
    • 0035271394 scopus 로고    scopus 로고
    • Vortical flowfield structure at forward swept-wing configurations
    • doi:10.2514/2.2758
    • Breitsamter, C., and Laschka, B., "Vortical Flowfield Structure at Forward Swept-Wing Configurations," Journal of Aircraft, Vol. 38, No. 2, 2001, pp. 193-207. doi:10.2514/2.2758
    • (2001) Journal of Aircraft , vol.38 , Issue.2 , pp. 193-207
    • Breitsamter, C.1    Laschka, B.2
  • 3
    • 0026106482 scopus 로고
    • Forward sweep: A favorable concept for a laminar flow wing
    • doi:10.2514/3.45997
    • Redeker, G., and Wichmann, G., "Forward Sweep: A Favorable Concept for a Laminar Flow Wing," Journal of Aircraft, Vol. 28, No. 2, 1991, pp. 97-103. doi:10.2514/3.45997
    • (1991) Journal of Aircraft , vol.28 , Issue.2 , pp. 97-103
    • Redeker, G.1    Wichmann, G.2
  • 4
    • 0033902353 scopus 로고    scopus 로고
    • The aerodynamic interaction at the junction between a forward-swept wing and a plate
    • Feb.
    • Arnott, A. D., and Bernstein, L., "The Aerodynamic Interaction at the Junction Between a Forward-Swept Wing and a Plate," The Aeronautical Journal, Vol. 104, No. 1032, Feb. 2000, pp. 67-88.
    • (2000) The Aeronautical Journal , vol.104 , Issue.1032 , pp. 67-88
    • Arnott, A.D.1    Bernstein, L.2
  • 5
    • 85003237312 scopus 로고
    • Simplified tunnel correction method
    • doi:10.2514/3.46705
    • Shindo, S., "Simplified Tunnel Correction Method," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 210-213. doi:10.2514/3.46705
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 210-213
    • Shindo, S.1
  • 9
    • 0015039667 scopus 로고
    • Prediction of vortex-lift characteristics by a leading edge suction analogy
    • doi:10.2514/3.44254
    • Polhamus, E. C., "Prediction of Vortex-Lift Characteristics by a Leading Edge Suction Analogy," Journal of Aircraft, Vol. 8, No. 4, 1971, pp. 193-199. doi:10.2514/3.44254
    • (1971) Journal of Aircraft , vol.8 , Issue.4 , pp. 193-199
    • Polhamus, E.C.1
  • 11
    • 0343425447 scopus 로고
    • Reciprocity relations in aerodynamics
    • Heaslet, M. A., and Spreiter, J. R., "Reciprocity Relations in Aerodynamics," NACA Rept. 1119, 1953, p. 16.
    • (1953) NACA Rept. 1119 , pp. 16
    • Heaslet, M.A.1    Spreiter, J.R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.