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001 9910713753103321
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035   $a(EXLCZ)995470000002504153
100   $a20190508d1952      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAchievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles /$fby J.C. Evvard and Lawrence R. Marcus
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1952.
215   $a1 online resource (8 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2616
300   $a"January 1952."
300   $a"[Prepared at] Lewis Flight Propulsion Laboratory... October 16, 1951"--Page 5.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aSupersonic nozzles$xDesign and construction
606   $aWind tunnels
606   $aSupersonic nozzles$xDesign and construction$2fast
606   $aWind tunnels$2fast
615  0$aSupersonic nozzles$xDesign and construction.
615  0$aWind tunnels.
615  7$aSupersonic nozzles$xDesign and construction.
615  7$aWind tunnels.
700   $aEvvard$b John C.$01423148
702   $aMarcus$b Lawrence R.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910713753103321
996   $aAchievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles$93549722
997   $aUNINA