Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface /

Bibliographic Details

Main Author:	Maksimov, V. P.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Maslov, A. A.
Format:	Government Document Microform Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, [1983]
Series:	NASA technical memorandum ; 77341.
Subjects:	Boundary layer control. Supersonic wind tunnels. Boundary layer transition. Flow stability. Surface cooling. Wall temperature. Wind tunnel nozzles. Wind tunnel walls.