02105oam 2200577 450 991071511140332120201231133853.0(CKB)5470000002508904(OCoLC)1139565367(EXLCZ)99547000000250890420200206d1932 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPreliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings /by Fred E. Weick and Carl J. WenzingerWashington, [D.C.] :National Advisory Committee for Aeronautics,1932.1 online resource (11 pages, 14 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 415"April, 1932."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).AerofoilsTestingSpoilers (Airplanes)Slotted flaps (Airplanes)Rolling (Aerodynamics)AerofoilsTestingfastRolling (Aerodynamics)fastSlotted flaps (Airplanes)fastSpoilers (Airplanes)fastAerofoilsTesting.Spoilers (Airplanes)Slotted flaps (Airplanes)Rolling (Aerodynamics)AerofoilsTesting.Rolling (Aerodynamics)Slotted flaps (Airplanes)Spoilers (Airplanes)Weick Fred E.1387817Wenzinger Carl J(Carl Joseph),1903-1988,United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715111403321Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings3463367UNINA