01479nam 2200397 a 450 991069702210332120230902161948.0(CKB)5470000002384684(OCoLC)710818237(EXLCZ)99547000000238468420110401d2005 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierApplication of computational fluid dynamics to a monoplane fixed-wing missile with elliptic cross sections[electronic resource] /by Karen Heavey and Jubaraj SahuAberdeen Proving Ground, MD :Army Research Laboratory,[2005]1 online resource (vi, 30 pages) color illustrationsARL-TR ;3549Title from title screen (viewed on Mar. 25, 2011)."July 2005."ARL-TR (Aberdeen Proving Ground, Md.) ;3549.Guided missilesAerodynamicsModelsFluid dynamicsModelsGuided missilesAerodynamicsModels.Fluid dynamicsModels.Heavey Karen R1414620Sahu Jabaraj1394996U.S. Army Research Laboratory.GPOGPOBOOK9910697022103321Application of computational fluid dynamics to a monoplane fixed-wing missile with elliptic cross sections3514470UNINA