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035   $a(EXLCZ)995470000002504761
100   $a20190508d1953      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 /$fby Paige B. Burbank and Robert W. Byrne
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1953.
215   $a1 online resource (37 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2921
300   $a"April 1953."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 11).
606   $aNozzles$xFluid dynamics
606   $aMach number
606   $aSupersonic nozzles$xDesign and construction
606   $aMach number$2fast
606   $aNozzles$xFluid dynamics$2fast
606   $aSupersonic nozzles$xDesign and construction$2fast
615  0$aNozzles$xFluid dynamics.
615  0$aMach number.
615  0$aSupersonic nozzles$xDesign and construction.
615  7$aMach number.
615  7$aNozzles$xFluid dynamics.
615  7$aSupersonic nozzles$xDesign and construction.
700   $aBurbank$b Paige B.$01421146
702   $aByrne$b Robert W.
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   $a9910713892903321
996   $aThe aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75$93541659
997   $aUNINA