Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
By: George T. Carson, Jr., and Francis J. Capone.
Contributors: Capone, Francis J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4237.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1991
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Format: Microform
Subjects: Axisymmetric flow.; Convergent-divergent nozzles.; Nozzle design.; Static tests.; Thrust vector control.; Transonic wind tunnels.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.