Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles
By: Ivan E. Beckwith and Barbara B. Holley
Contributors: Holley, Barbara B; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 1869
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 69
Subjects: Supersonic wind tunnels; Boundary layer
Notes: "Langley Research Center."

"August 1981"--Cover

Includes bibliographical references