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

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Bibliographic Details
Author / Creator:	Mason, Mary L., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, April 1986.
Description:	1 online resource (54 pages) : illustrations.
Language:	English
Series:	NASA/TP ; 2559 NASA technical paper ; 2559.
Subject:	Jet nozzles -- Testing. Airplanes -- Motors -- Thrust. Pitching (Aerodynamics) Short take-off and landing aircraft. Airplanes -- Motors -- Thrust. Jet nozzles -- Testing. Pitching (Aerodynamics) Short take-off and landing aircraft.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11665277

Hidden Bibliographic Details
Other authors / contributors:	Burley, James R., author. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body. Langley Research Center.
Notes:	"April 1986." Includes bibliographical references (pages 13-14). Technical paper. Langley Research Center L-16052 505-62-91-01 Description based on online resource, PDF version; title from title page (NASA, viewed July 11, 2018).
Other form:	Print version: Mason, Mary L Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability Microfiche: Mason, Mary L Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:2559

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