NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Acoustic prediction methods for rocket engines, including the effects of clustered engines and deflected exhaust flowAcoustic prediction methods for rocket engines
Document ID
19660030602
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Crocker, M. J.
(Wyle Labs., Inc. Huntsville, AL, United States)
Potter, R. C.
(Wyle Labs., Inc. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Physics, General
Report/Patent Number
NASA-CR-566
Accession Number
66N39892
Funding Number(s)
CONTRACT_GRANT: NAS8-11071
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
ACOUSTICS
No Preview Available