LEADER 01744nam  2200469I  450 
001 9910712818703321
005 20200210084732.0
035   $a(CKB)5470000002497999
035   $a(OCoLC)1140071522
035   $a(EXLCZ)995470000002497999
100   $a20200210j202001    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCold-flow model tests to determine static performance of a NASA one-sided ejector nozzle system /$fAlan S. Estenson and Timothy J. McDonald
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJanuary 2020.
215   $a1 online resource (x, 50 pages) $cillustrations (mostly color)
225 1 $aNASA/CR ;$v2020-220453
300   $a"January 2020."
320   $aIncludes bibliographical references (page 18).
517 3 $aCold-flow model tests to determine static performance of a National Aeronautics and Space Administration one-sided ejector nozzle system
606   $aCold flow tests$2nasat
606   $aInformation flow$2nasat
606   $aPhotonics$2nasat
606   $aEjectors$2nasat
606   $aPressure distribution$2nasat
615  7$aCold flow tests.
615  7$aInformation flow.
615  7$aPhotonics.
615  7$aEjectors.
615  7$aPressure distribution.
700   $aEstenson$b Alan S.$01408095
702   $aMcDonald$b Timothy J.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910712818703321
996   $aCold-flow model tests to determine static performance of a NASA one-sided ejector nozzle system$93491174
997   $aUNINA