A Reference Temperature Method for Compressible Laminar Boundary Layers
1973 ◽
Vol 2
(4)
◽
pp. 201-204
Keyword(s):
A calculation procedure for the solution of two-dimensional and axi-symmetric laminar boundary layers in compressible flow has been developed. The method is an extension of the integral approach of Tani to include compressibility effects by means of a reference temperature. Arbitrary pressure gradients and wall temperature can be specified. Comparisons with experiments obtained for supersonic flows over a flat plate indicate that the method yields adequate results. The method is then applied to the solution of the boundary layer on a Basemann inlet.
1967 ◽
Vol 29
(1)
◽
pp. 187-199
◽
1987 ◽
Vol 179
◽
pp. 469-487
◽
1993 ◽
Vol 246
◽
pp. 503-527
◽
Keyword(s):
2009 ◽
Vol 623
◽
pp. 273-282
◽
1983 ◽
Vol 387
(1793)
◽
pp. 331-349
◽
Keyword(s):
Keyword(s):