01017cam2 2200301 450 E60020007300220210909101009.020110324d1986 |||||ita|0103 baitaIT2LinguaggioFilosofiaPaul ValéryA cura di Judith Robinson-ValéryMilanoAdelphi Edizionic1986X, 447 p.22 cmBiblioteca Adelphi173001LAEC000159212001 *Biblioteca Adelphi173001E6002000729992000 QuaderniValéry, PaulAF00006229070343147Robinson-Valéry, JudithAF00022614070ITUNISOB20210909RICAUNISOBUNISOB84067194E600200073002M 102 Monografia moderna SBNM840001017-2Si67194AcquistovittoriniUNISOBUNISOB20110324075811.020151023131759.0AlfanoFilosofia169769021697689UNISOB02036nam 2200517 450 991070250830332120141203131305.0(CKB)5470000002429100(OCoLC)897378723(EXLCZ)99547000000242910020141203j201312 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierDefining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2) /Christopher A. SnyderCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,December 2013.1 online resource (10 pages) color illustrationsNASA/TM ;2013-218101Title from title screen (viewed on Dec. 3, 2014)."December 2013.""Prepared for the 67th Annual Forum and Technology Display (FORUM 67) sponsored by the American Helicopter Society International (AHS), Virginia Beach, Virginia, May 3-5, 2011."Includes bibliographical references (page 10).Defining gas turbine engine performance requirements for the Large Civil TiltRotor Tilt rotor aircraftnasatRotary wing aircraftnasatGas turbine enginesnasatRotor speednasatVertical takeoffnasatTilting rotorsnasatTilt rotor aircraft.Rotary wing aircraft.Gas turbine engines.Rotor speed.Vertical takeoff.Tilting rotors.Snyder Christopher A.1403483NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910702508303321Defining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2)3476947UNINA