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Volumn 17, Issue 6, 2001, Pages 1222-1226

Experimental study of scramjet module

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBERS; COMBUSTORS; FUEL INJECTION; HYDROCARBONS; HYDROGEN FUELS; IGNITION; INTAKE SYSTEMS; PERFORMANCE; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; THREE DIMENSIONAL; WIND TUNNELS;

EID: 0035509613     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5867     Document Type: Article
Times cited : (9)

References (7)
  • 3
    • 0006945217 scopus 로고
    • Design and experimental investigations of the convergent inlet configuration with 3D flow combinations
    • Preprint 30-83, Inst. of Theoretical and Applied Mechanics, Siberian Branch, Novosibirsk, Russia; (in Russian)
    • (1983)
    • Gutov, B.I.1    Zatoloka, V.V.2
  • 4
    • 0006900497 scopus 로고
    • Inlet performance of the integrated langley scramjet module (Mach 2.3 to 7.6)
    • AIAA Paper 75-1212, Oct
    • (1975)
    • Trexler, C.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.