NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Noise suppressor for turbofan-jet enginesExhaust nozzle equipped with bypass separators is basis of lightweight device. Innovation does not reduce thrust unduly and has no moving parts.
Document ID
19760000375
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Cheng, D. Y.
(Santa Clara Univ.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
Report Number: ARC-10812
ISSN: 0145-319X
ARC-10812
Accession Number
76B10375
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available