An Experimental Investigation Of Thrust Vectoring Two Dimensional Convergent Divergent Nozzles Installed In A Twin Engine Fighter Model At High Angles Of Attack

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Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept

Author	: David J. Wing
Publisher	:
Total Pages	: 132
Release	: 1994
ISBN-10	: NASA:31769000447303
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept by : David J. Wing

Download or read book Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept written by David J. Wing and published by . This book was released on 1994 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: