LEADER 02351oam  2200601I  450 
001 9910707497903321
005 20160809095639.0
035   $a(CKB)5470000002464545
035   $a(OCoLC)227848445
035   $a(EXLCZ)995470000002464545
100   $a20080512j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aThree-dimensional flow field measurements in a transonic turbine cascade /$fP.W. Giel [and seven others]
210  1$aCleveland, Ohio :$cNASA Lewis Research Center : U.S. Army Research Laboratory,$dDecember 1996.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107388
225 1 $aArmy Research Laboratory technical report ;$vARL-TR-1252
300   $aTitle from title screen (viewed Aug. 9, 2016).
300   $a"December 1996"--Report documentation page.
300   $a"Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996."
300   $a"Performing organization: NASA Lewis Research Center and U.S. Army Research Laboratory"--Report documentation page.
320   $aIncludes bibliographical references (page 14).
606   $aThree dimensional flow$2nasat
606   $aTurbine blades$2nasat
606   $aCascade flow$2nasat
606   $aFlow distribution$2nasat
606   $aTransonic flow$2nasat
606   $aRotor aerodynamics$2nasat
606   $aPressure distribution$2nasat
606   $aWind tunnel tests$2nasat
615  7$aThree dimensional flow.
615  7$aTurbine blades.
615  7$aCascade flow.
615  7$aFlow distribution.
615  7$aTransonic flow.
615  7$aRotor aerodynamics.
615  7$aPressure distribution.
615  7$aWind tunnel tests.
700   $aGiel$b P. W$g(Paul W.),$01390071
712 02$aLewis Research Center,
712 02$aU.S. Army Research Laboratory,
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707497903321
996   $aThree-dimensional flow field measurements in a transonic turbine cascade$93442388
997   $aUNINA