The paper considers the variational problem on minimization of convective heat flux transferred from a heated laminar boundary layer in a supersonic flow to a streamlined surface.
On Optimum Coolant Injection into a Laminar Boundary Layer in Supersonic Gas Flows
Russ. Aeronaut.
Russian Aeronautics ; 66 , 2 ; 252-258
01.04.2023
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Application of LDV to Supersonic Laminar Boundary Layer Flows
British Library Conference Proceedings | 1993
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