NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Evaluation of jet engine noiseThree basic equations, acoustic mode and two Mach modes, characterize jet noise environments. These equations are used to predict noise generation magnitude.
Document ID
19720000263
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Pao, S. P. (Wyle Labs.)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Physical Sciences
Report/Patent Number
MFS-21416
Report Number: MFS-21416
Accession Number
72B10263
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available