Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing.

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Bibliographic Details
Online Access:	Click here to view paper online
Main Author:	Wing, David J.
Corporate Author:	Langley Research Center
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, [1998]
Series:	NASA technical paper ; 206912.
Subjects:	Thrust vector control. Nozzle geometry. Convergent nozzles. Angular distribution. Flow distribution. Flapping. Pitch (Inclination)

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Holdings details from Online
Call Number:	NAS 1.60:206912
NAS 1.60:206912	Available

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.60:206912
NAS 1.60:206912	Restricted Place a Hold