02170oam 2200637 450 991071655230332120210623103328.0(CKB)5470000002522632(OCoLC)761140144(EXLCZ)99547000000252263220111115j197012 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of shortening transition liner to decrease overall length of a ram induction combustor /by Donald F. Schultz, Porter J. Perkins, and Jerrold D. WearWashington, D.C. :National Aeronautics and Space Administration,December 1970.1 online resource (18 pages) illustrationsNASA/TN ;D-7021"December 1970."Includes bibliographical references (pages 17-18).Turbojet enginesnasatCombustion chambersnasatAirplanesTurbojet enginesCombustionSmokeCombustionResearchAirplanesTurbojet enginesCombustionfastCombustion chambersTestingfastCombustionResearchfastSmokefastTurbojet engines.Combustion chambers.AirplanesTurbojet enginesCombustion.Smoke.CombustionResearch.AirplanesTurbojet enginesCombustion.Combustion chambersTesting.CombustionResearch.Smoke.Schultz Donald F.2680Perkins Porter J.Wear Jerrold D.United States.National Aeronautics and Space Administration,Lewis Research Center.OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910716552303321Effect of shortening transition liner to decrease overall length of a ram induction combustor3495894UNINA