02157nam 2200589 a 450 991069708720332120230902161639.0(CKB)5470000002384026(OCoLC)747715224(EXLCZ)99547000000238402620110824d2009 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCompressor study to meet large civil tilt rotor engine requirements[electronic resource] /Joseph P. Veres ; prepared for the 65th Annual Forum and Technology Display sponsored by the American Helicopter Society, Grapevine, Texas, May 27-29, 2009Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2009]1 online resource (35 pages) illustrationsNASA TM ;2009-215641Title from title screen (viewed on Aug. 24, 2011)."August 2009."Includes bibliographical references (page 35).NASA technical memorandum ;215641.CompressorsnasatTurbocompressorsnasatTilt rotor aircraftnasatLeading edgesnasatRotary wing aircraftnasatEngine designnasatFlow velocitynasatCentrifugal forcenasatTrailing edgesnasatCompressors.Turbocompressors.Tilt rotor aircraft.Leading edges.Rotary wing aircraft.Engine design.Flow velocity.Centrifugal force.Trailing edges.Veres Joseph P1386375Henriksen Stephen1386376NASA Glenn Research Center.AHS Forum and Technology Display(65th :2009 :Grapevine, Tex.)GPOGPOBOOK9910697087203321Compressor study to meet large civil tilt rotor engine requirements3435269UNINA