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035   $a(OCoLC)1159597614
035   $a(EXLCZ)995470000002524843
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine /$fby Sherod L. Earle and Francis J. Dutee
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (13 pages, 13 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 610
300   $a"August 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 13).
606   $aAirplanes$xMotors
606   $aAircraft gas-turbines$xCombustion chambers
606   $aTwo-stroke cycle engines
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAircraft gas-turbines$xCombustion chambers$2fast
606   $aAirplanes$xMotors$2fast
606   $aTwo-stroke cycle engines$2fast
615  0$aAirplanes$xMotors.
615  0$aAircraft gas-turbines$xCombustion chambers.
615  0$aTwo-stroke cycle engines.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAircraft gas-turbines$xCombustion chambers.
615  7$aAirplanes$xMotors.
615  7$aTwo-stroke cycle engines.
700   $aEarle$b Sherod L.$01391550
702   $aDutee$b Francis J.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716733503321
996   $aEffect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine$93445422
997   $aUNINA