Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
By: David J. Wing.
Contributors: Langley Research Center.
Series: [NASA technical paper] -- NASA/TP-1998-206912.; NASA technical paper -- 206912.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Thrust vector control.; Nozzle geometry.; Convergent nozzles.; Angular distribution.; Flow distribution.; Flapping.; Pitch (Inclination)
Notes: Shipping list no.: 99-0479-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 2 microfiches.