Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model
By: Francis J. Capone
Contributors: Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2044
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 77
Subjects: Jet nozzles
Notes: "Langley Research Center."

"August 1982"--Cover

Includes bibliographical references