Theoretical study of nonadiabatic boundary-layer stabilization times in a cryogenic wind tunnel for typical stainless-steel wing and fuselage models
By: Charles B. Johnson
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical memorandum -- 80212
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 42
Subjects: Heat -- Transmission
Notes: "Langley Research Center."

"July 1980"--Cover

Includes bibliographical references