01898nam 2200493I 450 991070424120332120160210101519.0(CKB)5470000002439264(OCoLC)938010487(EXLCZ)99547000000243926420160210j201509 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAn 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 /Reid A. Berdanier and Nicole L. KeyCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,September 2015.1 online resource (xiv, 145 pages) color illustrationsNASA/CR ;2015-218868Title from title screen (viewed Feb. 10, 2016)."September 2015.""Prepared under contract NNX11AI59A."Includes bibliographical references (pages 141-145).Wall flownasatTurbocompressorsnasatFlow visualizationnasatLeakagenasatTurbomachinerynasatWall flow.Turbocompressors.Flow visualization.Leakage.Turbomachinery.Berdanier Reid A.1390425Key Nicole L.NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910704241203321An 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 compressor3443099UNINA