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035   $a(CKB)5470000002439264
035   $a(OCoLC)938010487
035   $a(EXLCZ)995470000002439264
100   $a20160210j201509    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor /$fReid A. Berdanier and Nicole L. Key
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dSeptember 2015.
215   $a1 online resource (xiv, 145 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2015-218868
300   $aTitle from title screen (viewed Feb. 10, 2016).
300   $a"September 2015."
300   $a"Prepared under contract NNX11AI59A."
320   $aIncludes bibliographical references (pages 141-145).
606   $aWall flow$2nasat
606   $aTurbocompressors$2nasat
606   $aFlow visualization$2nasat
606   $aLeakage$2nasat
606   $aTurbomachinery$2nasat
615  7$aWall flow.
615  7$aTurbocompressors.
615  7$aFlow visualization.
615  7$aLeakage.
615  7$aTurbomachinery.
700   $aBerdanier$b Reid A.$01390425
702   $aKey$b Nicole L.
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704241203321
996   $aAn experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor$93443099
997   $aUNINA