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

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

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Bibliographic Details
Main Authors:	Mason, Mary L. (Author), Burley, James R. (Author)
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, April 1986
Series:	NASA technical paper ; 2559 NASA technical paper 2559
Subjects:	Airplanes > Motors > Thrust > ^A991136 Airplanes > Motors > Thrust Jet nozzles > Testing Pitching (Aerodynamics) > ^A1049530 Pitching (Aerodynamics) Short take-off and landing aircraft > ^A1060931 Short take-off and landing aircraft Afterburning Axisymmetric flow Nozzle geometry Nozzle thrust coefficients Static tests
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