Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
By: Robert J. Foley, Odis C. Pendergraft, Jr.
Contributors: Pendergraft, Odis C.; Langley Research Center.
Series: NASA technical paper -- 3085.
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
Number of pages: 77
Subjects: Convergent-divergent nozzles.; Jet vanes.; Nozzle geometry.; Static tests.; Static thrust.; Thrust vector control.; Yaw.; Jet nozzles -- Testing.; Blades.; Yawing (Aerodynamics); Airplanes -- Motors -- Thrust.
Notes: Prepared at Langley Research Center.

Bibliography: p. 11.

Microfiche. Washington, D.C. : National Aeronautics and Space Administration, 1991. 2 microfiche.