LEADER 01655oam  2200457Ia 450 
001 9910699379003321
005 20230902162205.0
035   $a(CKB)5470000002402123
035   $a(OCoLC)546918206
035   $a(EXLCZ)995470000002402123
100   $a20100308d2009      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFoil bearing starting considerations and requirements for rotorcraft engine applications$b[electronic resource] /$fby Kevin C. Radil and Christopher DellaCorte
210  1$aCleveland, OH :$cArmy Research Laboratory, NASA-Glenn Research Center,$d[2009]
215   $a1 online resource (iv, 14 pages) $cdigital, PDF file
225 1 $aARL-TR ;$v4873
300   $aTitle from title screen (viewed Mar. 5, 2010).
300   $a"August 2009."
320   $aIncludes bibliographical references (page 12).
410  0$aARL-TR (Aberdeen Proving Ground, Md.) ;$v4873.
606   $aGas-lubricated bearings
606   $aTurbomachines$xPerformance
606   $aRotors (Helicopters)
615  0$aGas-lubricated bearings.
615  0$aTurbomachines$xPerformance.
615  0$aRotors (Helicopters)
700   $aRadil$b Kevin C$01396149
701   $aDellaCorte$b Christopher$01386701
712 02$aNASA Glenn Research Center.
712 02$aU.S. Army Research Laboratory.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910699379003321
996   $aFoil bearing starting considerations and requirements for rotorcraft engine applications$93502738
997   $aUNINA