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Volumn 15, Issue 10, 1977, Pages 1455-1461

Wall cooling effects on hypersonic transitional/turbulent boundary layers at high Reynolds numbers

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS - HYPERSONIC;

EID: 0017545053     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.7440     Document Type: Article
Times cited : (17)

References (34)
  • 1
    • 84958445831 scopus 로고
    • Equilibrium Layers and Wall Turbulence
    • Townsend, A.A., “Equilibrium Layers and Wall Turbulence,”Journal of Fluid Mechanics, Vol. 11,1961, pp. 97-120.
    • (1961) Journal of Fluid Mechanics , vol.11 , pp. 97-120
    • Townsend, A.A.1
  • 4
    • 84959714668 scopus 로고
    • A Note on von Karmans Constant in Low Reynolds Number Turbulent Flows,”
    • Huffman, G.D. and Bradshaw, P., “A Note on von Karman’s Constant in Low Reynolds Number Turbulent Flows,”Journal of Fluid Mechanics, Vol. 53, Pt. 1, 1972, pp. 45-60.
    • (1972) Journal of Fluid Mechanics , vol.53 , pp. 45-60
    • Huffman, G.D.1    Bradshaw, P.2
  • 5
    • 85003268647 scopus 로고
    • Kinematic Eddy Viscosity at Low Reynolds Numbers
    • Cebeci, T., “Kinematic Eddy Viscosity at Low Reynolds Numbers,”AIAA Journal, Vol. 11, Jan. 1973, pp. 102-104.
    • (1973) AIAA Journal , vol.11 , pp. 102-104
    • Cebeci, T.1
  • 6
    • 85008283472 scopus 로고
    • Temperature Distributions in Supersonic Turbulent Boundary Layers
    • Nov
    • Meier, H.E. and Rotta, J.C., “Temperature Distributions in Supersonic Turbulent Boundary Layers,”AIAA Journal, Vol. 9, Nov. 1971, pp. 2149-2156.
    • (1971) AIAA Journal , vol.9 , pp. 2149-2156
    • Meier, H.E.1    Rotta, J.C.2
  • 7
    • 85007665427 scopus 로고
    • Calculation Methods for Compressible Turbulent Boundary Layers
    • (AGARD) Lecture Series on Compressible Turbulent Boundary Layers, Rhode-St. Genese, Belgium, March 1-5
    • Bushnell, D.M., Cary, A.M., Jr., and Harris, J.E., “Calculation Methods for Compressible Turbulent Boundary Layers,”Lecture Notes for von Karman Institute for Fluid Dynamics(AGARD) Lecture Series on Compressible Turbulent Boundary Layers, Rhode-St. Genese, Belgium, March 1-5, 1976.
    • (1976) Lecture Notes for Von Karman Institute for Fluid Dynamics
    • Bushnell, D.M.1    Cary, A.M.2    Harris, J.E.3
  • 9
    • 0014835270 scopus 로고
    • Calculation of Nonequilibrium Hypersonic Turbulent Boundary Layers and Comparisons with Experimental Data
    • Aug
    • Bushnell, D.M. and Beckwith, I.E., “Calculation of Nonequilibrium Hypersonic Turbulent Boundary Layers and Comparisons with Experimental Data,”AIAA Journal, Vol. 8, Aug. 1970, pp. 1462-1469.
    • (1970) AIAA Journal , vol.8 , pp. 1462-1469
    • Bushnell, D.M.1    Beckwith, I.E.2
  • 11
    • 0015615481 scopus 로고
    • Calculation of Transitional Boundary Layer Flows
    • April
    • Bushnell, D.M. and Alston, D.W., “Calculation of Transitional Boundary Layer Flows,”AIAA Journal, Vol. 11, April 1973, pp. 554-556.
    • (1973) AIAA Journal , vol.11 , pp. 554-556
    • Bushnell, D.M.1    Alston, D.W.2
  • 12
    • 0015434641 scopus 로고
    • Turbulent Properties of a Compressible Boundary Layer
    • Nov
    • Horstman, C.C. and Owen, F.K., “Turbulent Properties of a Compressible Boundary Layer,”AIAA Journal, Vol. 10, Nov. 1972, pp. 1418-1424.
    • (1972) AIAA Journal , vol.10 , pp. 1418-1424
    • Horstman, C.C.1    Owen, F.K.2
  • 14
    • 0015722634 scopus 로고
    • Hot-Wire Coil Probe for High Speed Flows
    • Weinstein, L.M., “Hot-Wire Coil Probe for High Speed Flows,”AIAA Journal, Vol. 11, Dec. 1973, pp. 1772-1773.
    • (1973) AIAA Journal , vol.11 , pp. 1772-1773
    • Weinstein, L.M.1
  • 16
    • 85003318512 scopus 로고
    • Influence of Moderate Wall Cooling on Cone Transition atMe= 13.7 in Helium
    • April
    • e= 13.7 in Helium,”Journal of Spacecraft and Rockets, Vol. 10, April 1973, pp. 282-283.
    • (1973) Journal of Spacecraft and Rockets , vol.10 , pp. 282-283
    • Fischer, M.C.1
  • 20
    • 84958438982 scopus 로고
    • The Drag of a Compressible Turbulent Boundary Layer on a Smooth Flat Plate With and Without Heat Transfer
    • Jan
    • Spalding, D.B. and Chi, S.W., “The Drag of a Compressible Turbulent Boundary Layer on a Smooth Flat Plate With and Without Heat Transfer,”Journal of Fluid Mechanics, Vol. 18, Pt. 1, Jan. 1964, pp. 117-143.
    • (1964) Journal of Fluid Mechanics , vol.18 , pp. 117-143
    • Spalding, D.B.1    Chi, S.W.2
  • 22
    • 0014747087 scopus 로고
    • Use of Coles Universal Wake Function for Compressible Turbulent Boundary Layers,”
    • March-April
    • Mathews, D.C., Childs, M.E., and Paynter, G.D., “Use of Coles’ Universal Wake Function for Compressible Turbulent Boundary Layers,”Journal of Aircraft, Vol. 7, March-April 1970, pp. 137-140.
    • (1970) Journal of Aircraft , vol.7 , pp. 137-140
    • Mathews, D.C.1    Childs, M.E.2    Paynter, G.D.3
  • 23
    • 85003208395 scopus 로고
    • Turbulent Boundary Layer in Compressible Fluids
    • van Driest, E.R., “Turbulent Boundary Layer in Compressible Fluids,”Journal of the Aeronautical Sciences, Vol. 18, 1951, pp. 145-160, p. 216.
    • (1951) Journal of the Aeronautical Sciences , vol.18
    • Van Driest, E.R.1
  • 29
    • 85003253432 scopus 로고
    • Entropy Layer Effects in Constant Pressure Hypersonic Boundary Layers
    • May
    • Sullivan, P.A. and Koziak, W.W., “Entropy Layer Effects in Constant Pressure Hypersonic Boundary Layers,”AIAA Journal, Vol. 11, May 1973, pp. 730-731.
    • (1973) AIAA Journal , vol.11 , pp. 730-731
    • Sullivan, P.A.1    Koziak, W.W.2
  • 31
    • 0016538352 scopus 로고
    • “Mixing Length in Low Reynolds Number Compressible Turbulent Boundary Layers
    • Aug
    • Bushnell, D.M., Cary, A.M., Jr., and Holley, B.B., “Mixing Length in Low Reynolds Number Compressible Turbulent Boundary Layers,” AIAA Journal, Vol. 13, Aug. 1975, pp. 1119-1121.
    • (1975) ” AIAA Journal , vol.13 , pp. 1119-1121
    • Bushnell, D.M.1    Cary, A.M.2    Holley, B.B.3
  • 34
    • 0015627856 scopus 로고
    • A Model for Eddy Conductivity and Turbulent Prandtl Number
    • May
    • Cebeci, T., “A Model for Eddy Conductivity and Turbulent Prandtl Number,”Journal of Heat Transfer, Vol. 95, May 1973, pp. 227-234.
    • (1973) Journal of Heat Transfer , vol.95 , pp. 227-234
    • Cebeci, T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.