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Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight, comprehensive data report. Volume 2: Laser velocimeter dataMean velocity (axial component) and turbulent velocity (axial component) measurements for thirty one selected flow conditions of six models were performed employing the Laser Doppler Velocimeter Aerodynamic conditions which define the test points are given. Tabulations which explain the scope of mean velocity traverses and turbulence histogram measurements are also presented. The actual LV position, the type of traverse, and measured mean and turbulent velocities along copies of the LV mean velocity traces are contained.
Document ID
19840025078
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
R82AEB491-VOL-2
NAS 1.26:168234-VOL-2
NASA-CR-168234-VOL-2
Accession Number
84N33149
Funding Number(s)
CONTRACT_GRANT: NAS3-22514
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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