LEADER 01479nam  2200397 a 450 
001 9910697022103321
005 20230902161948.0
035   $a(CKB)5470000002384684
035   $a(OCoLC)710818237
035   $a(EXLCZ)995470000002384684
100   $a20110401d2005      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of computational fluid dynamics to a monoplane fixed-wing missile with elliptic cross sections$b[electronic resource] /$fby Karen Heavey and Jubaraj Sahu
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2005]
215   $a1 online resource (vi, 30 pages) $ccolor illustrations
225 1 $aARL-TR ;$v3549
300   $aTitle from title screen (viewed on Mar. 25, 2011).
300   $a"July 2005."
410  0$aARL-TR (Aberdeen Proving Ground, Md.) ;$v3549.
606   $aGuided missiles$xAerodynamics$xModels
606   $aFluid dynamics$xModels
615  0$aGuided missiles$xAerodynamics$xModels.
615  0$aFluid dynamics$xModels.
700   $aHeavey$b Karen R$01414620
701   $aSahu$b Jabaraj$01394996
712 02$aU.S. Army Research Laboratory.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697022103321
996   $aApplication of computational fluid dynamics to a monoplane fixed-wing missile with elliptic cross sections$93514470
997   $aUNINA