02302oam 2200661 450 991071691110332120211130102354.0(CKB)5470000002527089(OCoLC)1145759772(EXLCZ)99547000000252708920200323d1934 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffect of retractable-spoiler location on rolling- and yawing-moment coefficents /J.A. ShortalWashington, [D.C.] :National Advisory Committee for Aeronautics,1934.1 online resource (12 pages, 5 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 499"July 1934."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 9).Spoilers (Airplanes)Flaps (Airplanes)AirplanesControl surfacesRolling (Aerodynamics)Yawing (Aerodynamics)Wind tunnel testingAirplanesControl surfacesfastFlaps (Airplanes)fastRolling (Aerodynamics)fastSpoilers (Airplanes)fastWind tunnel testingfastYawing (Aerodynamics)fastSpoilers (Airplanes)Flaps (Airplanes)AirplanesControl surfaces.Rolling (Aerodynamics)Yawing (Aerodynamics)Wind tunnel testing.AirplanesControl surfaces.Flaps (Airplanes)Rolling (Aerodynamics)Spoilers (Airplanes)Wind tunnel testing.Yawing (Aerodynamics)Shortal Joseph Adams1908-1409460United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716911103321Effect of retractable-spoiler location on rolling- and yawing-moment coefficents3495932UNINA