Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4̥ to 1.2 / Francis J. Capone ; Langley Research Center, Hampton, Va.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Capone, Francis J.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976.
Series:	NASA technical memorandum ; X-3313.
Subjects:	Airplanes > Jet propulsion. Nozzles > Testing.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3313
NAS 1.15:3313	Available Place a Hold