Theoretical study of laminar boundary layer on airfoil immersed in hypersonic stream is made under given assumption; numerical applications illustrate use of theory for flow along flat plate and for flow along curved wall for which shape is specified by certain governing profile parameters. Translation from Aerotecnica (Italy) Apr 1956 p 68-94.
Laminar boundary layer at hypersonic speeds
NASA -- Tech Translation
1961
56 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The laminar boundary layer at hypersonic speeds
TIBKAT | 1961
|Laminar boundary-layer growth on slightly blunted cones at hypersonic speeds
Engineering Index Backfile | 1965
|Turbulent boundary layer growth at hypersonic speeds
TIBKAT | 1973
|