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035   $a(CKB)5470000002429100
035   $a(OCoLC)897378723
035   $a(EXLCZ)995470000002429100
100   $a20141203j201312    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDefining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2) /$fChristopher A. Snyder
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2013.
215   $a1 online resource (10 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-218101
300   $aTitle from title screen (viewed on Dec. 3, 2014).
300   $a"December 2013."
300   $a"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."
320   $aIncludes bibliographical references (page 10).
517   $aDefining gas turbine engine performance requirements for the Large Civil TiltRotor 
606   $aTilt rotor aircraft$2nasat
606   $aRotary wing aircraft$2nasat
606   $aGas turbine engines$2nasat
606   $aRotor speed$2nasat
606   $aVertical takeoff$2nasat
606   $aTilting rotors$2nasat
615  7$aTilt rotor aircraft.
615  7$aRotary wing aircraft.
615  7$aGas turbine engines.
615  7$aRotor speed.
615  7$aVertical takeoff.
615  7$aTilting rotors.
700   $aSnyder$b Christopher A.$01403483
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702508303321
996   $aDefining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2)$93476947
997   $aUNINA