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Noise trends of a 0.5 m (20 in.) diameter supersonic throughflow fan as measured in an unmodified compressor aerodynamic test facility

By Dittmar, James H.

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Book Id: WPLBN0002209851
Format Type: PDF eBook :
File Size: 4.3 MB
Reproduction Date: 2012
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Title: Noise trends of a 0.5 m (20 in.) diameter supersonic throughflow fan as measured in an unmodified compressor aerodynamic test facility  
Author: Dittmar, James H.
Volume:
Language: English
Subject: AEROSPACE ENGINEERING, DATA BASES, EARTH SCIENCES
Collections: NASA Publication Collection
Historic
Publication Date:
1993
Publisher:

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H, D. J., D, M. R., & G, H. D. (1993). Noise trends of a 0.5 m (20 in.) diameter supersonic throughflow fan as measured in an unmodified compressor aerodynamic test facility. Retrieved from http://www.nationalpubliclibrary.info/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; The tone noise levels of a supersonic throughflow fan were measured at subsonic and supersonic axial duct Mach numbers. The noise in the inl

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: AEROSPACE ENGINEERING; DATA BASES; EARTH SCIENCES; DATA SYSTEMS; REMOTE SENSING; REMOTE SENSORS; LABORATORIES; RESEARCH AND DEVELOPMENT; SYSTEMS ENGINEERING; TECHNOLOGY UTILIZATION; AIRBORNE EQUIPMENT; BATHYMETERS

 

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