Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude
By: David M. Straight and Richard R. Cullom
Contributors: Cullom, Richard R; Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2171
Publisher: National Aeronautics and Space Administration Scieentific 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: 36
Subjects: Airplanes -- Turbojet engines; Airplanes -- Flight testing; Airplanes -- Motors -- Thrust
Notes: "Lewis Research Center."

Distributed to depository libraries in microfiche

"June 1983"--Cover

STAR category 07

Includes bibliographical references