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011430558 |
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20141009010000.0 |
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961018s1974 dcua b f000 0 eng d |
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‡asdr-uiuc6384377
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‡a(OCoLC)35762128
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‡aABC
‡cABC
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‡aUIUU
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4 |
‡aTL521.3.C6
‡bA3 no. 2436
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‡aNAS 1.26:2436
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‡aPfenninger, W.
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‡aReduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /
‡cby W. Pfenninger and J. Syberg.
|
260 |
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‡aWashington, D.C. :
‡bNational Aeronautics and Space Administration ;
‡a[Springfield, Va. :
‡bFor sale by the National Technical Information Service],
‡c1974.
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‡aiii, 303 p. :
‡bill. ;
‡c27 cm.
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‡aNASA contractor report ;
‡vNASA CR-2436
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‡a"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."
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‡aCover title.
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504 |
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‡aIncludes bibliographical references (p. 86-92).
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538 |
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‡aMode of access: Internet.
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‡aLaminar flow.
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‡aBoundary layer.
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‡aJet nozzles
‡xNoise.
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‡aSupersonic wind tunnels.
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‡aSyberg, J.
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‡aLangley Research Center.
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710 |
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‡aBoeing Commercial Airplane Company.
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‡a011430558
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‡a20101026084804.0
‡b20141009010000.0
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‡a20141112164151.0
‡b2023-03-14T18:17:54Z
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‡aSDR-UIUC
‡dUNKNOWN
‡lloader.pl-003-020
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‡aBK
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‡0sdr-uiuc6384377
‡auiug
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‡puiug.30112106582825
‡sUIU
‡16384377
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‡bUIU
‡cUIUC
‡d20230314
‡sgoogle
‡uuiug.30112106582825
‡y1974
‡rpd
‡qbib
‡tUS fed doc--NTIS: pubdate < 2018
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