LEADER 02157nam  2200589 a 450 
001 9910697087203321
005 20230902161639.0
035   $a(CKB)5470000002384026
035   $a(OCoLC)747715224
035   $a(EXLCZ)995470000002384026
100   $a20110824d2009      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCompressor study to meet large civil tilt rotor engine requirements$b[electronic resource] /$fJoseph P. Veres ; prepared for the 65th Annual Forum and Technology Display sponsored by the American Helicopter Society, Grapevine, Texas, May 27-29, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (35 pages) $cillustrations
225 1 $aNASA TM ;$v2009-215641
300   $aTitle from title screen (viewed on Aug. 24, 2011).
300   $a"August 2009."
320   $aIncludes bibliographical references (page 35).
410  0$aNASA technical memorandum ;$v215641.
606   $aCompressors$2nasat
606   $aTurbocompressors$2nasat
606   $aTilt rotor aircraft$2nasat
606   $aLeading edges$2nasat
606   $aRotary wing aircraft$2nasat
606   $aEngine design$2nasat
606   $aFlow velocity$2nasat
606   $aCentrifugal force$2nasat
606   $aTrailing edges$2nasat
615  7$aCompressors.
615  7$aTurbocompressors.
615  7$aTilt rotor aircraft.
615  7$aLeading edges.
615  7$aRotary wing aircraft.
615  7$aEngine design.
615  7$aFlow velocity.
615  7$aCentrifugal force.
615  7$aTrailing edges.
700   $aVeres$b Joseph P$01386375
701   $aHenriksen$b Stephen$01386376
712 02$aNASA Glenn Research Center.
712 12$aAHS Forum and Technology Display$d(65th :$f2009 :$eGrapevine, Tex.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697087203321
996   $aCompressor study to meet large civil tilt rotor engine requirements$93435269
997   $aUNINA