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Volumn 38, Issue 9, 2000, Pages 1754-1755

Effect of total temperature on boundary-layer stability at Mach 6

Author keywords

[No Author keywords available]

Indexed keywords

HYPERSONIC FLOW; THERMAL EFFECTS;

EID: 0034275339     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1164     Document Type: Article
Times cited : (7)

References (15)
  • 1
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    • (1959) Handbuch der Physik , vol.8 , pp. 243-246
    • Serrin, J.1
  • 2
    • 0003242679 scopus 로고
    • Stability of axisymmetric boundary layers on sharp cones at hypersonic mach numbers
    • June
    • Mack, L. M., "Stability of Axisymmetric Boundary Layers on Sharp Cones at Hypersonic Mach Numbers," AIAA Paper 87-1413, June 1987.
    • (1987) AIAA Paper 87-1413
    • Mack, L.M.1
  • 3
    • 0002608606 scopus 로고
    • On the inviscid acoustic-mode instability of supersonic shear flows part 1: Two-dimensional waves
    • Mack, L. M., "On the Inviscid Acoustic-Mode Instability of Supersonic Shear Flows Part 1: Two-Dimensional Waves," Theoretical and Computational Fluid Dynamics, Vol. 2, 1990, pp. 97-123.
    • (1990) Theoretical and Computational Fluid Dynamics , vol.2 , pp. 97-123
    • Mack, L.M.1
  • 4
    • 0015617093 scopus 로고
    • Influence of total temperature on transition in supersonic flow
    • Ross, R., "Influence of Total Temperature on Transition in Supersonic Flow," AIAA Journal, Vol. 11, No. 4, 1973, pp. 563-565.
    • (1973) AIAA Journal , vol.11 , Issue.4 , pp. 563-565
    • Ross, R.1
  • 6
    • 0004731518 scopus 로고
    • A review of freestream flow fluctuation and steady-state flow quality measurements in the AEDC/VKF supersonic tunnel A and hypersonic tunnel B
    • April
    • Donaldson, J., and Coulter, S., "A Review of Freestream Flow Fluctuation and Steady-State Flow Quality Measurements in the AEDC/VKF Supersonic Tunnel A and Hypersonic Tunnel B," AIAA Paper 95-6137, April 1995.
    • (1995) AIAA Paper 95-6137
    • Donaldson, J.1    Coulter, S.2
  • 7
    • 85007035453 scopus 로고
    • Laminar boundary-layer stability experiments on a cone at mach 8, part 5: Tests with a cooled model
    • June
    • Stetson, K. F., Thompson, E. R., Donaldson, J. C., and Siler, L. G., "Laminar Boundary-Layer Stability Experiments on a Cone at Mach 8, Part 5: Tests with a Cooled Model," AIAA Paper 89-1895, June 1989.
    • (1989) AIAA Paper 89-1895
    • Stetson, K.F.1    Thompson, E.R.2    Donaldson, J.C.3    Siler, L.G.4
  • 9
    • 0026981575 scopus 로고
    • Example of second-mode instability dominance at a mach number of 5.2
    • Stetson, K. F., and Kimmel, R. L., "Example of Second-Mode Instability Dominance at a Mach Number of 5.2," AIAA Journal, Vol. 30, No. 12, 1992, pp. 2974-2976.
    • (1992) AIAA Journal , vol.30 , Issue.12 , pp. 2974-2976
    • Stetson, K.F.1    Kimmel, R.L.2
  • 11
    • 0031095583 scopus 로고    scopus 로고
    • The effect of pressure gradients on transition zone length in hypersonic boundary layers
    • Kimmel, R. L., "The Effect of Pressure Gradients on Transition Zone Length in Hypersonic Boundary Layers," Journal of Fluids Engineering, Vol. 119, No. 1, 1997, pp. 36-41.
    • (1997) Journal of Fluids Engineering , vol.119 , Issue.1 , pp. 36-41
    • Kimmel, R.L.1
  • 12
    • 0003308715 scopus 로고
    • Laminar boundary-layer stability experiments on a cone at mach 8, part 1: Sharp cone
    • July
    • Stetson, K. F., Thompson, E. R., Donaldson, J. C., and Siler, L. G., "Laminar Boundary-Layer Stability Experiments on a Cone at Mach 8, Part 1: Sharp Cone," AIAA Paper 83-1761, July 1983.
    • (1983) AIAA Paper 83-1761
    • Stetson, K.F.1    Thompson, E.R.2    Donaldson, J.C.3    Siler, L.G.4
  • 13
    • 0030405648 scopus 로고    scopus 로고
    • Boundary-layer stability measurements in a hypersonic quiet tunnel
    • Lachowicz, J. T., Chokani, N., and Wilkinson, S. P., "Boundary-Layer Stability Measurements in a Hypersonic Quiet Tunnel," AIAA Journal, Vol. 34, No. 12, 1996, pp. 2496-2500.
    • (1996) AIAA Journal , vol.34 , Issue.12 , pp. 2496-2500
    • Lachowicz, J.T.1    Chokani, N.2    Wilkinson, S.P.3
  • 15
    • 0034275339 scopus 로고    scopus 로고
    • Effect of total temperature on boundary layer stability at mach 6
    • Jan.
    • Kimmel, R. L., and Poggie, J., "Effect of Total Temperature on Boundary Layer Stability at Mach 6," AIAA Paper 99-0816, Jan. 1999.
    • (1999) AIAA Paper 99-0816
    • Kimmel, R.L.1    Poggie, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.