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Volumn , Issue , 2001, Pages

Computational study of support influence on base flow of a model in supersonic flow

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894467713     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (11)
  • 6
    • 84894331996 scopus 로고
    • Experimental investigation on the effect of tail surfaces and angle of attack on base pressure in supersonic flow
    • AGARD CP10
    • Heyser, A., Maurer, F. and Oberdorffer, E., Experimental investigation on the effect of tail surfaces and angle of attack on base pressure in supersonic flow, in: The Fluid Dynamic Aspects of Ballistics, AGARD CP10, 1966.
    • (1966) The Fluid Dynamic Aspects of Ballistics
    • Heyser, A.1    Maurer, F.2    Oberdorffer, E.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.