Inlet noise studies for an axial-flow single-stage compressor

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035 ‡a(OCoLC)63515121
040 ‡aEGM ‡cEGM
049 ‡aUIUU
090 ‡aTN D-2615
100 1 ‡aCopeland, W. Latham.
245 1 0 ‡aInlet noise studies for an axial-flow single-stage compressor / ‡cW. Latham Copeland.
246 3 ‡aNASA TN D-2615
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], ‡c1965.
300 ‡a19 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vD-2615
504 ‡aIncludes bibliographical references (p. 7).
538 ‡aMode of access: Internet.
650 0 ‡aCompressors ‡xAerodynamics.
650 0 ‡aCompressors ‡xNoise.
650 0 ‡aAxial flow compressors.
710 2 ‡aLangley Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011447725
DAT 0 ‡a20101103082721.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2024-01-23T18:45:27Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
HOL ‡0sdr-uiuc6392410 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106868109 ‡sUIU ‡16392410
974 ‡bUIU ‡cUIUC ‡d20240123 ‡sgoogle ‡uuiug.30112106868109 ‡y1965 ‡ric ‡qbib ‡tUS bib date1 >= 1929