NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Spoiler-generated flow noise. II.Analytical model of spoiler generated sound in jet pipe, presenting data on level, spectrum and directivity of sound
Document ID
19690041473
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gordon, C. G.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Subject Category
Physics, General
Accession Number
69A19462
Distribution Limits
Public
Copyright
Other

Available Downloads

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