LEADER 01545oam  2200433Ia 450 
001 9910699944503321
005 20110317095743.0
035   $a(CKB)5470000002406512
035   $a(OCoLC)74252465
035   $a(EXLCZ)995470000002406512
100   $a20080513d2003      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPrediction of projectile performance, stability, and free-flight motion using computational fluid dynamics$b[electronic resource] /$fPaul Weinacht
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2003]
215   $a1 online resource (iv, 26 pages) $cillustrations
225 1 $aARL-TR ;$v3015
300   $aTitle from title screen (viewed on Mar. 17, 2011).
300   $a"July 2003."
320   $aIncludes bibliographical references (pages 20-21).
606   $aTrajectories (Mechanics)
606   $aProjectiles, Aerial$xAerodynamics
606   $aComputational fluid dynamics
615  0$aTrajectories (Mechanics)
615  0$aProjectiles, Aerial$xAerodynamics.
615  0$aComputational fluid dynamics.
700   $aWeinacht$b P$01391971
712 02$aU.S. Army Research Laboratory.
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910699944503321
996   $aPrediction of projectile performance, stability, and free-flight motion using computational fluid dynamics$93462374
997   $aUNINA