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INVESTIGATION OF ADJUSTABLE SUPERSONIC INLET IN COMBINATION WITH J34 ENGINE UP TO MACH 2.0

By Leissler, L. A.

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Book Id: WPLBN0002196650
Format Type: PDF eBook :
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Reproduction Date: 2012
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Title: INVESTIGATION OF ADJUSTABLE SUPERSONIC INLET IN COMBINATION WITH J34 ENGINE UP TO MACH 2.0  
Author: Leissler, L. A.
Volume:
Language: English
Subject: ADJUSTING, J-34 ENGINE, BYPASSES
Collections: NASA Publication Collection
Historic
Publication Date:
20012
Publisher:

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A, L. L., & C, N. J. (20012). INVESTIGATION OF ADJUSTABLE SUPERSONIC INLET IN COMBINATION WITH J34 ENGINE UP TO MACH 2.0. Retrieved from http://www.netlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: ADJUSTING; J-34 ENGINE; BYPASSES; TURBOJET ENGINE; PRESSURE RECOVERY; SUPERSONIC INLET; COWLINGS; INTERCEPTION; J-34 ENGINE; MACH NUMBER; PRESSURE RECOVERY; SUPERSONIC INLETS; TURBOJET ENGINES

 

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