Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

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Bibliographic Details
Main Author:	Carson, George T.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Capone, Francis J.
Format:	Government Document Microfilm Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1991.
Series:	NASA technical memorandum ; 4237.
Subjects:	Axisymmetric flow. Convergent-divergent nozzles. Nozzle design. Static tests. Thrust vector control. Transonic wind tunnels. Wind tunnel tests.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:4237
NAS 1.15:4237	Restricted Place a Hold