Turbulent-flow separation criteria for overexpanded supersonic nozzles
By: E. Leon Morisette and Theordore J. Goldberg, Langley Research Center
Contributors: Goldberg, Theodore J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper ; 1207
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 36
Subjects: Turbulent boundary layer; Stratified flow; Supersonic nozzles
Notes: Issued Aug. 1978

Includes bibliographical references