02140oam 2200577 450 991071673350332120210825124814.0(CKB)5470000002524843(OCoLC)1159597614(EXLCZ)99547000000252484320200623d1937 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine /by Sherod L. Earle and Francis J. DuteeWashington, [D.C.] :National Advisory Committee for Aeronautics,1937.1 online resource (13 pages, 13 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 610"August 1937."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 13).AirplanesMotorsAircraft gas-turbinesCombustion chambersTwo-stroke cycle enginesAeronauticsResearchAeronauticsResearchfastAircraft gas-turbinesCombustion chambersfastAirplanesMotorsfastTwo-stroke cycle enginesfastAirplanesMotors.Aircraft gas-turbinesCombustion chambers.Two-stroke cycle engines.AeronauticsResearch.AeronauticsResearch.Aircraft gas-turbinesCombustion chambers.AirplanesMotors.Two-stroke cycle engines.Earle Sherod L.1391550Dutee Francis J.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716733503321Effect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine3445422UNINA