Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
By: Mary L. Mason and James R. Burley II.
Contributors: Burley, James R.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2559.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1986
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Motors -- Thrust.; Jet nozzles -- Testing.; Pitching (Aerodynamics); Short take-off and landing aircraft.; Axisymmetric flow.; Nozzle geometry.; Nozzle thrust coefficients.; Short takeoff aircraft.; Static tests.; Thrust vector control.
Notes: Includes bibliographical references.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1986. 1 microfiche.