Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /

Bibliographic Details
Main Authors:	Mason, Mary L. (Author), Burley, James R. (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, April 1986.
Series:	NASA technical paper ; 2559.
Subjects:	Nozzle geometry. Static tests. Nozzle thrust coefficients. Axisymmetric flow. Afterburning. Jet nozzles > Testing. Airplanes > Motors > Thrust. Pitching (Aerodynamics) Short take-off and landing aircraft.
Online Access:	https://purl.fdlp.gov/GPO/gpo105627

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