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Advanced Subsonic Technology Separate Flow Nozzle Tests for Engine Noise Reduction Sub-ElementContents of this presentation include Baseline configurations for all models.
Document ID
20010037749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saiyed, Naseem H. (NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 20, 2013
Publication Date
December 1, 2000
Publication Information
Publication: Separate Flow Nozzle Test Status Meeting
Subject Category
Acoustics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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