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Treated inletsDesign of lined ring inlet for reduced noise sound pressure levels of Boeing 707 aircraft engine
Document ID
19690002224
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Drakeley, G. T.
(Boeing Co. Seattle, WA, United States)
Mc Cormick, R. B.
(Boeing Co. Seattle, WA, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1968
Publication Information
Publication: NASA PROGR. OF NASA RES. RELATING TO NOISE ALLEVIATION OF LARGE SUBSONIC JET AIRCRAFT 1968
Subject Category
Aircraft
Accession Number
69N11555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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