Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Simpson, Roger L
1971.
The effect of a discontinuity in wall blowing on the turbulent incompressible boundary layer.
International Journal of Heat and Mass Transfer,
Vol. 14,
Issue. 12,
p.
2083.
Bradshaw, P.
and
Ferriss, D. H.
1971.
Calculation of boundary-layer development using the turbulent energy equation: compressible flow on adiabatic walls.
Journal of Fluid Mechanics,
Vol. 46,
Issue. 1,
p.
83.
BUSHNELL, D. M.
and
MORRIS, D. J.
1971.
Eddy viscosity distributions in a Mach 20 turbulent boundary layer.
AIAA Journal,
Vol. 9,
Issue. 4,
p.
764.
Huffman, G. David
and
Bradshaw, Peter
1972.
A note on von Kármán's constant in low Reynolds number turbulent flows.
Journal of Fluid Mechanics,
Vol. 53,
Issue. 01,
p.
45.
Glazkov, V. V.
Guseva, M. D.
and
Zhestkov, B. A.
1972.
Turbulent flow over permeable plates.
Fluid Dynamics,
Vol. 7,
Issue. 4,
p.
569.
Landis, R.B
and
Mills, A.F
1972.
The calculation of turbulent boundary layers with foreign gas injection.
International Journal of Heat and Mass Transfer,
Vol. 15,
Issue. 10,
p.
1905.
Kays, W.M
1972.
Heat transfer to the transpired turbulent boundary layer.
International Journal of Heat and Mass Transfer,
Vol. 15,
Issue. 5,
p.
1023.
HORSTMAN, C. C.
and
OWEN, F. K.
1972.
Turbulent properties of a compressible boundary layer..
AIAA Journal,
Vol. 10,
Issue. 11,
p.
1418.
Rekin, A. D.
1972.
Velocity profile in a turbulent boundary layer of a supersonic gas stream.
Journal of Engineering Physics,
Vol. 23,
Issue. 1,
p.
883.
BUSHNELL, D. M.
and
ALSTON, D. W.
1973.
Calculation of transitional boundary-layer flows..
AIAA Journal,
Vol. 11,
Issue. 4,
p.
554.
GERHART, PHILIP M.
1973.
Heat transfer downstream of attachment of a turbulent supersonic shear layer..
AIAA Journal,
Vol. 11,
Issue. 1,
p.
104.
CEBECI, TUNCER
1973.
Kinematic eddy viscosity at low Reynolds numbers..
AIAA Journal,
Vol. 11,
Issue. 1,
p.
102.
Afzal, Noor
1973.
A higher order theory for compressible turbulent boundary layers at moderately large Reynolds number.
Journal of Fluid Mechanics,
Vol. 57,
Issue. 1,
p.
1.
Baker, R.J.
and
Launder, B.E.
1974.
The turbulent boundary layer with foreign gas injection—II. Predictions and measurements in severe streamwise pressure gradients.
International Journal of Heat and Mass Transfer,
Vol. 17,
Issue. 2,
p.
293.
WASSEL, A. T.
and
MILLS, A. F.
1974.
Combustion of carbon particles in a hypersonic turbulent boundary layer.
Journal of Spacecraft and Rockets,
Vol. 11,
Issue. 12,
p.
803.
1974.
Analysis of Turbulent Boundary Layers.
Vol. 15,
Issue. ,
p.
385.
Bushnell, D. M.
Cary, A. M.
and
Holley, B. B.
1975.
Mixing Length in Low Reynolds Number Compressible Turbulent Boundary Layers.
AIAA Journal,
Vol. 13,
Issue. 8,
p.
1119.
Adams, J. C.
1975.
Low Reynolds number effect on hypersonic lifting body turbulent boundary layers.
Journal of Spacecraft and Rockets,
Vol. 12,
Issue. 2,
p.
126.
Galbraith, R A McD
and
Head, M R
1975.
Eddy Viscosity and Mixing Length from Measured Boundary Layer Developments.
Aeronautical Quarterly,
Vol. 26,
Issue. 2,
p.
133.
Antonia, Robert A.
and
Beck, Robert E.
1975.
Turbulent Boundary Layers with Wall Injection.
AIAA Journal,
Vol. 13,
Issue. 7,
p.
952.