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Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight, comprehensive data report. Volume 3: Shadowgraph photos and facility descriptionA total of 142 shadowgraph photographs were taken on 43 different plumes that were distributed over the six nozzle configurations using the 9.5 inch diameter collimated light beam of the shadowgraph setup. Aerodynamic flow conditions of the shadowgraph test points, the location and identification of each of the photographs, and copies of the pictures are presented.
Document ID
19840025079
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yamamoto, K. (General Electric Co. Cincinnati, OH, United States)
Brausch, J. F. (General Electric Co. Cincinnati, OH, United States)
Janardan, B. A. (General Electric Co. Cincinnati, OH, United States)
Hoerst, D. J. (General Electric Co. Cincinnati, OH, United States)
Price, A. O. (General Electric Co. Cincinnati, OH, United States)
Knott, P. R. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:168234-VOL-3
NASA-CR-168234-VOL-3
R82AEB491-VOL-3
Accession Number
84N33150
Funding Number(s)
CONTRACT_GRANT: NAS3-22514
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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