Optimal pitch thrust-vector angle and benefits for all flight regimes /

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Bibliographic Details
Author / Creator:	Gilyard, Glenn B., author.
Imprint:	Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, March 2000.
Description:	1 online resource (22 pages) : illustrations.
Language:	English
Series:	NASA/TM ; 2000-209021 NASA technical memorandum ; 2000-209021.
Subject:	Aerodynamics. Airplanes -- Motors -- Thrust. Drag (Aerodynamics) Lift (Aerodynamics)
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11552959

Hidden Bibliographic Details
Other authors / contributors:	Bolonkin, Alexander, author. Hugh L. Dryden Flight Research Center, issuing body.
Notes:	"March 2000." "Performing organization: NASA Dryden Flight Research Center"--Report documentation page. Includes bibliographical references (page 22). Technical memorandum. Sponsored by the National Aeronautics and Space Administration WU 522-16-14-00-39-00-LIO H-2402 Description based on online resource; title from PDF title page (NASA, viewed Oct. 23, 2017).
Other form:	Print version: Gilyard, Glenn B. Optimal pitch thrust-vector angle and benefits for all flight regimes Microfiche version: Gilyard, Glenn B. Optimal pitch thrust-vector angle and benefits for all flight regimes
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:209021

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