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Volumn , Issue , 1997, Pages

A review of hypersonic boundary layer stability experiments in a quiet mach 6 wind tunnel

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FLUID DYNAMICS; HYPERSONIC BOUNDARY LAYERS; HYPERSONIC FLOW; STABILITY;

EID: 0039660599     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (30)
  • 4
    • 0027238977 scopus 로고
    • Experimental Transition Zone Lengths in Pressure Gradient in Hypersonic Flow, in ASME FED
    • Kimmel, R.L.: Experimental Transition Zone Lengths in Pressure Gradient in Hypersonic Flow, in ASME FED Vol. 151, Transitional and Turbulent Compressible Flows, 1993, pp 117-127.
    • (1993) Transitional and Turbulent Compressible Flows , vol.151 , pp. 117-127
    • Kimmel, R.L.1
  • 5
    • 2842545690 scopus 로고
    • Effect of Adverse Pressure Gradient on the Second Mode Instability in Hypersonic Boundary Layers
    • Hampton, VA, Report No. HTC-9006, December
    • Malik, M.R., Balakumar P. and Chang, C.-L.: Effect of Adverse Pressure Gradient on the Second Mode Instability in Hypersonic Boundary Layers, High Technology Corporation, Hampton, VA, Report No. HTC-9006, December, 1990.
    • (1990) High Technology Corporation
    • Malik, M.R.1    Balakumar, P.2    Chang, C.-L.3
  • 6
    • 0342819149 scopus 로고
    • EMalik: A New Spatial Stability Analysis Program for Transition Prediction Using the eN Method
    • Hampton, VA, Report No. HTC-9203
    • Malik, M.R.: eMalik: A New Spatial Stability Analysis Program for Transition Prediction Using the eN Method. High Technology Corporation, Hampton, VA, Report No. HTC-9203, 1992.
    • (1992) High Technology Corporation
    • Malik, M.R.1
  • 7
    • 0037995942 scopus 로고
    • Effect of Adverse Pressure Gradient and Wall Cooling on Instability of Hypersonic Boundary Layers
    • Hampton, VA, Report No. HTC-9404, March
    • Balakumar P. and Malik M.R.: Effect of Adverse Pressure Gradient and Wall Cooling on Instability of Hypersonic Boundary Layers, High Technology Corporation, Hampton, VA, Report No. HTC-9404, March, 1994.
    • (1994) High Technology Corporation
    • Balakumar, P.1    Malik, M.R.2
  • 8
    • 34249753851 scopus 로고
    • Spatial Direct Numerical Simulation of Highspeed Boundary-layer Flows - Part II: Transition on a Cone in Mach 8 Flow
    • Pruett C.D. and Chang C.-L.: Spatial Direct Numerical Simulation of Highspeed Boundary-layer Flows - Part II: Transition on a Cone in Mach 8 Flow, Theoretical and Computational Fluid Dynamics, Vol. 7, No. 5, 1995, pp 397-423.
    • (1995) Theoretical and Computational Fluid Dynamics , vol.7 , Issue.5 , pp. 397-423
    • Pruett, C.D.1    Chang, C.-L.2
  • 10
    • 0030824502 scopus 로고    scopus 로고
    • NASA Langley Mach 6 Quiet Wind- Tunnel Performance
    • January
    • Blanchard A.E., Lachowicz JT and Wilkinson S.P.: NASA Langley Mach 6 Quiet Wind- Tunnel Performance, AIAA Journal, Vol. 35, No. 1, January, 1997, pp 23-28.
    • (1997) AIAA Journal , vol.35 , Issue.1 , pp. 23-28
    • Blanchard, A.E.1    Lachowicz, J.T.2    Wilkinson, S.P.3
  • 12
    • 0030405648 scopus 로고    scopus 로고
    • Boundary-Layer Stability Measurements in a Hypersonic Quiet Tunnel
    • December
    • Lachowicz J.T., Chokani N. and Wilkinson S.P.: Boundary-Layer Stability Measurements in a Hypersonic Quiet Tunnel, AIAA Journal, Vol. 34, No. 12, December, 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
  • 16
    • 0010113810 scopus 로고    scopus 로고
    • Effect of Angel of Attack on Hypersonic Boundary-Layer Stability
    • March
    • Doggett, G.P., Chokani N. and Wilkinson S.P.: Effect of Angel of Attack on Hypersonic Boundary-Layer Stability, AIAA Journal, Vol. 35, No. 3, March, 1997, pp.464-470.
    • (1997) AIAA Journal , vol.35 , Issue.3 , pp. 464-470
    • Doggett, G.P.1    Chokani, N.2    Wilkinson, S.P.3
  • 25
    • 0027260175 scopus 로고
    • Analysis of a Constant Voltage Anemometer Circuit
    • Irvine, CA, May
    • Sarma, G.R.: Analysis of a Constant Voltage Anemometer Circuit, IEEE/IMTC Conference, Irvine, CA, May, 1993.
    • (1993) IEEE/IMTC Conference
    • Sarma, G.R.1
  • 27
    • 3342968776 scopus 로고    scopus 로고
    • A Comparative Study of Constant-Voltage and Constant-Temperature Hot-Wire Anemometers in Supersonic Flow
    • Kegerise M.A. and Spina E.F.: A Comparative Study of Constant-Voltage and Constant-Temperature Hot-Wire Anemometers in Supersonic Flow, ASME FED, Vol. 239, 1996, pp. 297-308
    • (1996) ASME FED , vol.239 , pp. 297-308
    • Kegerise, M.A.1    Spina, E.F.2
  • 28
    • 0016483098 scopus 로고
    • Linear Stability Theory and the Problem of Supersonic Boundary-Layer Transition
    • March
    • Mack L.M.: Linear Stability Theory and the Problem of Supersonic Boundary-Layer Transition, AIAA Journal Vol. 13, No. 3, March, 1975, Pp 278-289.
    • (1975) AIAA Journal , vol.13 , Issue.3 , pp. 278-289
    • Mack, L.M.1
  • 29
    • 0016483071 scopus 로고
    • Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition
    • Kendall, J.M.: Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition, AIAA Journal Vol. 13, No. 3, 1975, pp. 290-299
    • (1975) AIAA Journal , vol.13 , Issue.3 , pp. 290-299
    • Kendall, J.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.