Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero
By: Lawrence E. Putnam and Edward G. Strong
Contributors: Strong, Edward G; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 85655
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 42
Subjects: Jet nozzles; Jet planes -- Thrust reversers
Notes: Distributed to depository libraries in microfiche

"December 1983"--Cover

Subject category 02

Includes bibliographical references