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Volumn 19, Issue 5, 2000, Pages 695-706

Transition studies on an elliptic cone in Mach 8 flow using filtered Rayleigh scattering

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CARBON DIOXIDE; FLOW OF FLUIDS; IMAGING TECHNIQUES; LASERS; RAYLEIGH SCATTERING; REYNOLDS NUMBER;

EID: 0034272410     PISSN: 09977546     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0997-7546(00)00130-8     Document Type: Article
Times cited : (38)

References (11)
  • 1
    • 0003076129 scopus 로고
    • Boundary-layer stability theory, Special course on stability and transition of laminar flow
    • Mack L.M., Boundary-layer stability theory, Special course on stability and transition of laminar flow, AGARD Report 709, 1984.
    • (1984) AGARD Report , vol.709
    • Mack, L.M.1
  • 4
    • 0021855811 scopus 로고
    • Laminar boundary-layer stability experiments on a cone at Mach 8, part 3: Sharp cone at angle of attack
    • Stetson K.F., Thompson E.R., Donaldson J.C., Siler L.G., Laminar boundary-layer stability experiments on a cone at Mach 8, part 3: Sharp cone at angle of attack, AIAA Paper 85-0492, 1985.
    • (1985) AIAA Paper 85-0492
    • Stetson, K.F.1    Thompson, E.R.2    Donaldson, J.C.3    Siler, L.G.4
  • 5
    • 84983134092 scopus 로고    scopus 로고
    • Traveling instabilities in elliptic cone boundary-layer transition at Mach 8
    • Poggie J., Kimmel R.L., Traveling instabilities in elliptic cone boundary-layer transition at Mach 8, AIAA Paper 98-0435, 1998.
    • (1998) AIAA Paper 98-0435
    • Poggie, J.1    Kimmel, R.L.2
  • 8
    • 0003297848 scopus 로고    scopus 로고
    • Quantitative visualization of supersonic flow using Rayleigh scattering
    • Poggie J., Smits A.J., Quantitative visualization of supersonic flow using Rayleigh scattering, AIAA Paper 96-0436, 1996.
    • (1996) AIAA Paper 96-0436
    • Poggie, J.1    Smits, A.J.2
  • 10
    • 0003295970 scopus 로고    scopus 로고
    • Three-dimensional hypersonic laminar boundary layer computations for transition experiment design
    • Kimmel R.L., Schwoerke S.N., Klein M.A., Three-dimensional hypersonic laminar boundary layer computations for transition experiment design, AIAA Paper 96-2080, 1996.
    • (1996) AIAA Paper 96-2080
    • Kimmel, R.L.1    Schwoerke, S.N.2    Klein, M.A.3
  • 11
    • 0007004314 scopus 로고
    • Use of transition correlations for three-dimensional boundary layers within hypersonic flows
    • Lyttle I.J., Reed H.S., Use of transition correlations for three-dimensional boundary layers within hypersonic flows, AIAA Paper 95-2293, 1995.
    • (1995) AIAA Paper 95-2293
    • Lyttle, I.J.1    Reed, H.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.