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Potential of inlet-guide-vane configuration for inlet noise reductionInlet guide vane configuration effects on axial flow compressor noise reduction
Document ID
19690002230
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Chestnutt, D. (NASA Langley Research Center Hampton, VA, United States)
Crigler, J. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Publication Information
Publication: PROGR. OF NASA RES. RELATING TO NOISE ALLEVIATION OF LARGE SUBSONIC JET AIRCRAFT 1968
Subject Category
Aircraft
Accession Number
69N11561
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19690002211Collected WorksProgress of NASA research relating to noise alleviation of large subsonic jet aircraftN69-11542 02-02Collected Works
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