LEADER 01929nam  2200469I  450 
001 9910706600403321
005 20171108075728.0
035   $a(CKB)5470000002456438
035   $a(OCoLC)1010746916
035   $a(EXLCZ)995470000002456438
100   $a20171108j200111    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aParametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet /$fRene? Fernandez [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dNovember 2001.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-107181
300   $a"November 2001."
300   $a"Prepared for the 1995 Airbreathing Propulsion Subcommittee Meeting sponsored by the Joint Army-Navy-NASA-Air Force Interagency Propulsion Committee, Tampa, Florida, December 5-9, 1995."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
320   $aIncludes bibliographical references (page 6).
606   $aScale models$2nasat
606   $aInlet pressure$2nasat
606   $aPerformance tests$2nasat
606   $aWind tunnel tests$2nasat
606   $aRocket-based combined-cycle engines$2nasat
615  7$aScale models.
615  7$aInlet pressure.
615  7$aPerformance tests.
615  7$aWind tunnel tests.
615  7$aRocket-based combined-cycle engines.
700   $aFernandez$b Rene?$01403136
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706600403321
996   $aParametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet$93475073
997   $aUNINA