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Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction

By Shaw, R. J.

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Book Id: WPLBN0002203094
Format Type: PDF eBook :
File Size: 3.9 MB
Reproduction Date: 2012
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Title: Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction  
Author: Shaw, R. J.
Volume:
Language: English
Subject: HUMAN REACTIONS, NOISE INTENSITY, BANDWIDTH
Collections: NASA Publication Collection
Historic
Publication Date:
1974
Publisher:

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J, S. R., W, S. B., & A, M. G. (1974). Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction. Retrieved from http://www.worldpubliclibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; The results of an experimental investigation to increase the stable airflow operating range of a supersonic mixed-compression inlet are pres

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: HUMAN REACTIONS; NOISE INTENSITY; BANDWIDTH; AUDIO FREQUENCIES; NOISE THRESHOLD; NOISE TOLERANCE; EFFECTIVE PERCEIVED NOISE LEVELS; HUMAN TOLERANCES

 

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