Subjective response to combined noise and vibration during flight of a large twin-jet airplane /

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050 4 ‡aTL521.3.T4 ‡bA3 no. 3406
086 0 ‡aNAS 1.15:X-3406
100 1 ‡aClevenson, Sherman A.
245 1 0 ‡aSubjective response to combined noise and vibration during flight of a large twin-jet airplane / ‡cSherman A. Clevenson ; Langley Research Center, Hampton, Va.
260 ‡aWashington : ‡bU.S. National Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1976.
300 ‡a[1], 41 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical memorandum ; ‡vNASA TM X-3406
500 ‡aCover title.
504 ‡aIncludes bibliographical references (p. 20).
538 ‡aMode of access: Internet.
650 0 ‡aAerodynamic noise.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
710 2 ‡aLangley Research Center.
CID ‡a011426537
DAT 0 ‡a20101007165349.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2016-10-07T19:17:42Z
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