Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane /

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Bibliographic Details
Author / Creator:	Kurtenbach, Frank J., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
Description:	1 online resource (18 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1782 NASA technical paper ; 1782.
Subject:	Airplanes -- Motors -- Thrust. Fighter planes -- Turbojet engines. Jet propulsion.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914287

Hidden Bibliographic Details
Other authors / contributors:	Burcham, Frank W., author. Hugh L. Dryden Flight Research Center. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	Title from title screen (viewed on Aug. 25, 2016). "January 1981." "Performing Organization: NASA Dryden Flight Research Center"--Report documentation page. Includes bibliographical references (page 18). Technical paper. National Aeronautics and Space Administration RTOP 506-51-34 RTOP 505-11-24 H-1118
Other form:	Print version: Kurtenbach, Frank J. Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane Microfiche version: Kurtenbach, Frank J. Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1782

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