메뉴 건너뛰기




Volumn 472, Issue , 2002, Pages 83-124

Experiments on stability and transition at Mach 3

Author keywords

[No Author keywords available]

Indexed keywords

LAMINAR FLOW; NOZZLES; REYNOLDS NUMBER;

EID: 0037059084     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112002002094     Document Type: Article
Times cited : (33)

References (45)
  • 11
    • 0000046943 scopus 로고
    • Secondary instability of high speed flows and the influence of wall cooling and suction
    • (1992) Phys. Fluids A , vol.4 , pp. 727-743
    • El-Hady, N.M.1
  • 18
    • 0016483071 scopus 로고
    • Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition
    • (1975) AIAA J , vol.13 , pp. 290-299
    • Kendall, J.M.1
  • 23
    • 0000541157 scopus 로고
    • Factors affecting transition Reynolds numbers on models in supersonic wind tunnels
    • (1954) J. Aero. Sci , vol.21 , pp. 497-498
    • Laufer, J.1
  • 25
    • 33748717393 scopus 로고
    • Some statistical properties of the radiated pressure field generated by a supersonic turbulent boundary layer
    • (1964) Phys. Fluids , vol.7 , pp. 1191-1197
    • Laufer, J.1
  • 30
    • 0016483098 scopus 로고
    • Linear stability theory and the problem of supersonic boundary-layer transition
    • (1975) AIAA J , vol.3 , pp. 278-289
    • Mack, L.M.1
  • 36
    • 85007654866 scopus 로고
    • Radiated aerodynamic noise effects on boundary layer transition in supersonic and hypersonic wind tunnels
    • (1969) AIAA J , vol.7 , pp. 450-457
    • Pate, S.R.1    Schueler, C.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.