LEADER 01753oam  2200541   450 
001 9910714093903321
005 20201102150434.0
035   $a(CKB)5470000002506729
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035   $a(EXLCZ)995470000002506729
100   $a20120408j196902    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTheoretical analysis of flow in VTOL lift fan inlets without crossflow /$fby Norbert O. Stockman and Seymour Lieblein
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dFebruary 1969.
215   $a1 online resource (ii, 37 pages) $cillustrations
225 1 $aNASA technical note ;$vNASA TN D-5065
300   $a"February 1969."
320   $aIncludes bibliographical references (pages 36-37).
606   $aVertically rising aircraft
606   $aLift fans
606   $aLift fans$2fast
606   $aVertically rising aircraft$2fast
615  0$aVertically rising aircraft.
615  0$aLift fans.
615  7$aLift fans.
615  7$aVertically rising aircraft.
700   $aStockman$b Norbert O.$01419401
702   $aLieblein$b Seymour
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bTRL
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714093903321
996   $aTheoretical analysis of flow in VTOL lift fan inlets without crossflow$93533708
997   $aUNINA