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035   $a(EXLCZ)995470000002385049
100   $a20110404d2004      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical investigation of aerodynamics of canard-controlled missile using planar and grid tail fins$hPart II$iSubsonic and transonic flow$b[electronic resource] /$fby James DeSpirito, Milton E. Vaughn, Jr., and W. David Washington
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2004]
215   $a1 online resource (x, 92 pages) $ccolor illustrations
225 1 $aARL-TR ;$v3162
300   $aTitle from title screen (viewed on Apr. 1, 2011).
300   $a"March 2004."
410  0$aARL-TR (Aberdeen Proving Ground, Md.) ;$v3162.
606   $aRockets (Aeronautics)$xCanard fins$xAerodynamics$xModels
606   $aRockets (Aeronautics)$xFins$xAerodynamics$xModels
615  0$aRockets (Aeronautics)$xCanard fins$xAerodynamics$xModels.
615  0$aRockets (Aeronautics)$xFins$xAerodynamics$xModels.
700   $aDeSpirito$b James$01400611
701   $aVaughn$b Milton E$01400612
701   $aWashington$b W. David$01400613
712 02$aU.S. Army Research Laboratory.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697186003321
996   $aNumerical investigation of aerodynamics of canard-controlled missile using planar and grid tail fins$93467858
997   $aUNINA