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On the design of acoustic liners for rocket engines - Helmholtz resonators evaluated with a rocket combustorHelmholtz resonators with variable cavity depths tested with unstable rocket combustor
Document ID
19690013986
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hannum, N. P. (NASA Lewis Research Center Cleveland, OH, United States)
Phillips, B. (NASA Lewis Research Center Cleveland, OH, United States)
Russell, L. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1969
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-5171
Accession Number
69N23351
Funding Number(s)
CONTRACT_GRANT: 128-31-06-05-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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