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035   $a(OCoLC)227960512
035   $a(EXLCZ)995470000002404666
100   $a20080513d2001      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBlack Hawk helicopter vibration analysis due to main rotor damage$b[electronic resource] $edirectional constituents of the resultant vibrations /$fby Joseph C. Fries
210  1$aAberdeen Proving Ground, MD :$cU.S. Army Research Laboratory,$d[2001]
215   $a1 online resource (viii, 16 pages) $cillustrations
225 1 $aARL-TR ;$v2442
300   $aTitle from title screen (viewed on Feb. 3, 2011).
300   $a"March 2001."
320   $aIncludes bibliographical references (page 9).
517   $aBlack Hawk helicopter vibration analysis due to main rotor damage 
606   $aBlack Hawk (Military transport helicopter)
606   $aVibration (Aeronautics)$xPhysiological effect
606   $aRotors (Helicopters)
615  0$aBlack Hawk (Military transport helicopter)
615  0$aVibration (Aeronautics)$xPhysiological effect.
615  0$aRotors (Helicopters)
700   $aFries$b Joseph C$01413966
712 02$aU.S. Army Research Laboratory.
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910699627303321
996   $aBlack Hawk helicopter vibration analysis due to main rotor damage$93511796
997   $aUNINA