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

Main Author: Kurtenbach, Frank J.,
Other Authors: Burcham, Frank W.,, Hugh L. Dryden Flight Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch,
Format: eBook
Language: English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
Physical Description: 1 online resource (18 pages) : illustrations.
Series: NASA technical paper ; 1782.
Online Access: https://purl.fdlp.gov/GPO/gpo71438
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245 1 0 |a Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane /  |c Frank J. Kurtenbach and Frank W. Burcham, Jr. 
264 1 |a [Washington, D.C.] :  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c January 1981. 
300 |a 1 online resource (18 pages) :  |b illustrations. 
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490 1 |a NASA technical paper ;  |v 1782. 
500 |a Title from title screen (viewed on Aug. 25, 2016). 
500 |a "January 1981." 
500 |a "Performing Organization: NASA Dryden Flight Research Center"--Report documentation page. 
500 |a GPO Cataloging Record Distribution Program (CRDP). 
504 |a Includes bibliographical references (page 18). 
513 |a Technical paper. 
536 |a National Aeronautics and Space Administration  |h RTOP 506-51-34. 
536 |d RTOP 505-11-24  |d H-1118. 
650 7 |a Afterburning.  |2 nasat. 
650 7 |a F-15 aircraft.  |2 nasat. 
650 7 |a Jet thrust.  |2 nasat. 
650 7 |a Pressure measurement.  |2 nasat. 
650 7 |a Turbofan engines.  |2 nasat. 
650 7 |a Airplanes  |x Motors  |x Thrust.  |2 fast. 
650 7 |a Fighter planes  |x Turbojet engines.  |2 fast. 
650 7 |a Jet propulsion.  |2 fast. 
655 7 |a Technical reports.  |2 lcgft. 
700 1 |a Burcham, Frank W.,  |e author. 
710 2 |a Hugh L. Dryden Flight Research Center. 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch,  |e issuing body. 
776 0 8 |i Print version:  |a Kurtenbach, Frank J.  |t Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane  |w (OCoLC)7324805. 
776 0 8 |i Microfiche version:  |a Kurtenbach, Frank J.  |t Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane  |w (OCoLC)711544701. 
830 0 |a NASA technical paper ;  |v 1782. 
856 4 0 |u https://purl.fdlp.gov/GPO/gpo71438 
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