01580oam 2200457 450 991071697130332120211103131201.0(CKB)5470000002526481(OCoLC)1282246460(OCoLC)995470000002526481(EXLCZ)99547000000252648120211103j196904 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierSensitivity of subsonic transport range to turbofan engine design /by Robert W. Koenig and Laurence H. Fishbach[Washington, D.C] :National Aeronautics and Space Administration,April 1969.1 online resource (approximately 20 pages) illustrationsNASA/TM ;X-52603"April 1969."Includes bibliographical references (page 10).Turbofan enginesnasatSubsonic flownasatDescent propulsion systemsnasatAscent propulsion systemsnasatTurbofan engines.Subsonic flow.Descent propulsion systems.Ascent propulsion systems.Koenig Robert W.1406898Fishbach Laurence H.United States.National Aeronautics and Space Administration,GPOGPOGPOBOOK9910716971303321Sensitivity of subsonic transport range to turbofan engine design3513042UNINA