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Volumn 39, Issue 12, 2001, Pages 2357-2365

Numerical analysis of reducing driver gas contamination in impulse shock tunnels

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTER SIMULATION; CONTACTS (FLUID MECHANICS); FINITE VOLUME METHOD; LAMINAR FLOW; NAVIER STOKES EQUATIONS; NOZZLES; SHOCK WAVES; UNSTEADY FLOW; VISCOUS FLOW; WIND TUNNELS;

EID: 0035662495     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1242     Document Type: Article
Times cited : (29)

References (22)
  • 4
    • 0018504531 scopus 로고
    • Interaction between the unsteady boundary layer and inviscid hot flow in a shock tube
    • (1979) AIAA Journal , vol.17 , Issue.8 , pp. 821-827
    • Zeitoun, D.1    Imbert, M.2
  • 5
    • 0003596675 scopus 로고
    • The interaction of a reflected shock with the boundary layer in a shock tube
    • March
    • (1958) NACA TM , vol.1418
    • Mark, H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.