-
1
-
-
84958445831
-
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
-
3
-
-
84882415693
-
-
NASATMX-2310, Aug
-
Bushnell, D.M. and Morris, D. J., “Shear Stress, Eddy Viscosity, and Mixing Length Distribution in Hypersonic Turbulent Boundary Layers,” NASATMX-2310, Aug. 1971.
-
(1971)
Shear Stress, Eddy Viscosity, and Mixing Length Distribution in Hypersonic Turbulent Boundary Layers
-
-
Bushnell, D.M.1
Morris, D.J.2
-
4
-
-
84959714668
-
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
-
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
-
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
-
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
-
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
-
10
-
-
3242842820
-
-
AIAA Paper 73-165, New York, Jan.10-12
-
Watson, R.D., Harris, J.E., and Anders, J.B., Jr., “Measurements in a Transitional/Turbulent Mach 10 Boundary Layer at High Reynolds Numbers,” AIAA Paper 73-165, New York, Jan.10-12, 1973.
-
(1973)
Measurements in a Transitional/Turbulent Mach 10 Boundary Layer at High Reynolds Numbers
-
-
Watson, R.D.1
Harris, J.E.2
Anders, J.B.3
-
11
-
-
0015615481
-
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
-
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
-
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
-
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
-
17
-
-
77949311414
-
-
Paper presented at Fluid Dynamics Panel Specialists’ Meeting, AGARD-CP-93, Sept. 13-15
-
Mabey, D.G., Meier, H.U., and Sawyer, W.G., “Some Boundary Layer Measurements on a Flat Plate at Mach Numbers from 2.5 to 4.5,” Paper presented at Fluid Dynamics Panel Specialists’ Meeting, AGARD-CP-93, Sept. 13-15, 1971.
-
(1971)
Some Boundary Layer Measurements on a Flat Plate at Mach Numbers from 2.5 to 4.5
-
-
Mabey, D.G.1
Meier, H.U.2
Sawyer, W.G.3
-
18
-
-
85003286113
-
-
NASA TN D-5433
-
Bushnell, D.M., Johnson, C.B., Harvey, W.D., and Feller, W.V., “Comparison of Prediction Methods and Studies of Relaxation in Hypersonic Turbulent Nozzle-Wall Boundary Layers,” NASA TN D-5433, 1969.
-
(1969)
Comparison of Prediction Methods and Studies of Relaxation in Hypersonic Turbulent Nozzle-Wall Boundary Layers
-
-
Bushnell, D.M.1
Johnson, C.B.2
Harvey, W.D.3
Feller, W.V.4
-
20
-
-
84958438982
-
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
-
21
-
-
0037758541
-
-
NASA TN D-5560, Jan
-
Cary, A.M., Jr., “Summary of Available Information on Reynolds Analogy for Zero-Pressure-Gradient, Compressible, Turbulent-Boundary-Layer Flow,” NASA TN D-5560, Jan. 1970.
-
(1970)
Summary of Available Information on Reynolds Analogy for Zero-Pressure-Gradient, Compressible, Turbulent-Boundary-Layer Flow
-
-
Cary, A.M.1
-
22
-
-
0014747087
-
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
-
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
-
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
-
“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
-
32
-
-
85003277857
-
-
Naval Ordnance Lab., 63-77, AD-422359, Oct
-
Tetervin, N., “A Semi-Empirical Derivation of Friction, Heat-Transfer, and Mass-Transfer Coefficients for the Constant Property Turbulent Boundary Layer on a Flat Plate,” Naval Ordnance Lab., 63-77, AD-422359, Oct. 1963.
-
(1963)
A Semi-Empirical Derivation of Friction, Heat-Transfer, and Mass-Transfer Coefficients for the Constant Property Turbulent Boundary Layer on a Flat Plate
-
-
Tetervin, N.1
-
34
-
-
0015627856
-
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
|