LEADER 01969nam  2200493I  450 
001 9910705782403321
005 20170908154307.0
035   $a(CKB)5470000002452580
035   $a(OCoLC)989980610
035   $a(EXLCZ)995470000002452580
100   $a20170613j199706    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical assessment of four-port through-flow wave rotor cycles with passage height variation /$fD.E. Paxson and Jules W. Lindau
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJune 1997.
215   $a1 online resource (12 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107490
300   $a"June 1997"--Report documentation page.
300   $a"Prepared for the 33rd Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Seattle, Washington, July 6-9, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"Report documentation page.
300   $a"AIAA-97-3142."
320   $aIncludes bibliographical references (pages 11-12).
606   $aComputational fluid dynamics$2nasat
606   $aFlow distribution$2nasat
606   $aFuel consumption$2nasat
606   $aGas turbine engines$2nasat
606   $aPressure ratio$2nasat
615  7$aComputational fluid dynamics.
615  7$aFlow distribution.
615  7$aFuel consumption.
615  7$aGas turbine engines.
615  7$aPressure ratio.
700   $aPaxson$b Daniel E.$01386438
702   $aLindau$b Jules W.
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705782403321
996   $aNumerical assessment of four-port through-flow wave rotor cycles with passage height variation$93475367
997   $aUNINA