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Volumn 37, Issue 1, 2000, Pages 189-192

Transonic and low-supersonic aerodynamic analysis of a wing with underpylon/store

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FIGHTER AIRCRAFT; PRESSURE DISTRIBUTION; SHOCK WAVES; STEADY FLOW; SUPERSONIC FLOW; TRANSONIC FLOW; UNSTEADY FLOW; WIND TUNNELS;

EID: 0033888852     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2582     Document Type: Article
Times cited : (13)

References (7)
  • 2
    • 0022026464 scopus 로고    scopus 로고
    • "An Efficient Coordinate Transformation Technique for Unsteady, Transonic Aerodynamic Analysis of Low Aspect-Ratio Wings,"
    • Guruswamy, G. P., and Goorjian, P. M., "An Efficient Coordinate Transformation Technique for Unsteady, Transonic Aerodynamic Analysis of Low Aspect-Ratio Wings," Journal of Aircraft, Vol. 22, No. 3,1985, pp. 193-199.
    • Journal of Aircraft, Vol. 22, No. 3,1985, Pp. 193-199.
    • Guruswamy, G.P.1    Goorjian, P.M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.