LEADER 01492oam  2200445Ia 450 
001 9910697248103321
005 20230902161648.0
035   $a(CKB)5470000002386442
035   $a(OCoLC)74252802
035   $a(EXLCZ)995470000002386442
100   $a20080513d2003      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn approximate method for pitch-damping prediction$b[electronic resource] /$fJames E. Danberg and Paul Weinacht
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2003]
215   $a1 online resource (1 volumes (various pagings)) $cdigital, PDF file
225 1 $aARL-TR ;$v3007
300   $aTitle from title screen (viewed Nov. 26, 2010).
300   $a"July 2003."
320   $aIncludes bibliographical references (pages 32-33).
410  0$aARL-TR (Aberdeen Proving Ground, Md.) ;$v3007.
606   $aAxial flow
606   $aAngle of attack (Aerodynamics)
606   $aFlight control
615  0$aAxial flow.
615  0$aAngle of attack (Aerodynamics)
615  0$aFlight control.
700   $aDanberg$b James E$01416541
701   $aWeinacht$b P$01391971
712 02$aU.S. Army Research Laboratory.
801  0$bDTICE
801  1$bDTICE
801  2$bGPO
906   $aBOOK
912   $a9910697248103321
996   $aAn approximate method for pitch-damping prediction$93522245
997   $aUNINA