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100   $a20190508d1952      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section /$fby Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1952.
215   $a1 online resource (30 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2711
300   $a"June 1952."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 18).
606   $aNozzles$xFluid dynamics
606   $aSupersonic nozzles$xDesign and construction
606   $aAxial flow
606   $aWind tunnel testing
606   $aMathematical analysis
606   $aAxial flow$2fast
606   $aMathematical analysis$2fast
606   $aNozzles$xFluid dynamics$2fast
606   $aSupersonic nozzles$xDesign and construction$2fast
606   $aWind tunnel testing$2fast
615  0$aNozzles$xFluid dynamics.
615  0$aSupersonic nozzles$xDesign and construction.
615  0$aAxial flow.
615  0$aWind tunnel testing.
615  0$aMathematical analysis.
615  7$aAxial flow.
615  7$aMathematical analysis.
615  7$aNozzles$xFluid dynamics.
615  7$aSupersonic nozzles$xDesign and construction.
615  7$aWind tunnel testing.
700   $aBeckwith$b Ivan E.$01403844
702   $aRidyard$b Herbert W.
702   $aCromer$b Nancy
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   $a9910713895903321
996   $aThe aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section$93521478
997   $aUNINA