02286oam 2200625 450 991071524380332120210126134341.0(CKB)5470000002509587(OCoLC)1143006492(EXLCZ)99547000000250958720200304d1933 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierRolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /by R.H. HealdWashington, [D.C.] :National Advisory Committee for Aeronautics,1933.1 online resource (12 pages, 3 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 441"January, 1933."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 12).Rolling, yawing, and hinge moments produced by rectangular ailerons AileronsFlaps (Airplanes)Rolling (Aerodynamics)Yawing (Aerodynamics)Hinge moments (Aerodynamics)Wind tunnel testingHinge moments (Aerodynamics)fastRolling (Aerodynamics)fastWind tunnel testingfastYawing (Aerodynamics)fastAilerons.Flaps (Airplanes)Rolling (Aerodynamics)Yawing (Aerodynamics)Hinge moments (Aerodynamics)Wind tunnel testing.Hinge moments (Aerodynamics)Rolling (Aerodynamics)Wind tunnel testing.Yawing (Aerodynamics)Heald R. H.1401601United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715243803321Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370)3488626UNINA