01492oam 2200445Ia 450 991069724810332120230902161648.0(CKB)5470000002386442(OCoLC)74252802(EXLCZ)99547000000238644220080513d2003 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAn approximate method for pitch-damping prediction[electronic resource] /James E. Danberg and Paul WeinachtAberdeen Proving Ground, MD :Army Research Laboratory,[2003]1 online resource (1 volumes (various pagings)) digital, PDF fileARL-TR ;3007Title from title screen (viewed Nov. 26, 2010)."July 2003."Includes bibliographical references (pages 32-33).ARL-TR (Aberdeen Proving Ground, Md.) ;3007.Axial flowAngle of attack (Aerodynamics)Flight controlAxial flow.Angle of attack (Aerodynamics)Flight control.Danberg James E1416541Weinacht P1391971U.S. Army Research Laboratory.DTICEDTICEGPOBOOK9910697248103321An approximate method for pitch-damping prediction3522245UNINA