02094oam 2200625 450 991071718630332120220118133843.0(CKB)5470000002528350(OCoLC)785096315(EXLCZ)99547000000252835020120408j197702 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffects of tip clearance on overall performance of transonic fan stage with and without casing treatment /Royce D. Moore and Walter M. OsbornWashington, D.C. :National Aeronautics and Space Administration,February 1977.1 online resource (approximately 27 pages) illustrationsNASA/TM ;X-3479"February 1977."Includes bibliographical references (page 7).CasingnasatTurbofan enginesnasatTransonic flownasatAerodynamics, TransonicfastAirplanesTurbofan enginesfastAirplanesTurbojet enginesBladesfastCompressorsAerodynamicsfastCompressorsBladesfastCasing.Turbofan engines.Transonic flow.Aerodynamics, Transonic.AirplanesTurbofan engines.AirplanesTurbojet enginesBlades.CompressorsAerodynamics.CompressorsBlades.Moore Royce D.1386958Osborn Walter M.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQOCLCOOCLCQOCLCOGPOBOOK9910717186303321Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment3436297UNINA