01681nam 2200409Ia 450 991069718600332120230902161858.0(CKB)5470000002385049(OCoLC)710978744(EXLCZ)99547000000238504920110404d2004 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierNumerical investigation of aerodynamics of canard-controlled missile using planar and grid tail finsPart IISubsonic and transonic flow[electronic resource] /by James DeSpirito, Milton E. Vaughn, Jr., and W. David WashingtonAberdeen Proving Ground, MD :Army Research Laboratory,[2004]1 online resource (x, 92 pages) color illustrationsARL-TR ;3162Title from title screen (viewed on Apr. 1, 2011)."March 2004."ARL-TR (Aberdeen Proving Ground, Md.) ;3162.Rockets (Aeronautics)Canard finsAerodynamicsModelsRockets (Aeronautics)FinsAerodynamicsModelsRockets (Aeronautics)Canard finsAerodynamicsModels.Rockets (Aeronautics)FinsAerodynamicsModels.DeSpirito James1400611Vaughn Milton E1400612Washington W. David1400613U.S. Army Research Laboratory.GPOGPOBOOK9910697186003321Numerical investigation of aerodynamics of canard-controlled missile using planar and grid tail fins3467858UNINA