02222oam 2200589 450 991071687940332120210920120858.0(CKB)5470000002525389(OCoLC)1159597651(EXLCZ)99547000000252538920200623d1938 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierInterference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps /by Albert ShermanWashington, [D.C.] :National Advisory Committee for Aeronautics,1938.1 online resource (9 pages, 7 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 640"March, 1938."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 7).AirplanesWingsTestingAirplanesFuselageTestingSplit flaps (Airplanes)Interference (Aerodynamics)Wind tunnel testingAirplanesFuselageTestingfastInterference (Aerodynamics)fastSplit flaps (Airplanes)fastWind tunnel testingfastAirplanesWingsTesting.AirplanesFuselageTesting.Split flaps (Airplanes)Interference (Aerodynamics)Wind tunnel testing.AirplanesFuselageTesting.Interference (Aerodynamics)Split flaps (Airplanes)Wind tunnel testing.Sherman Albert1386917United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716879403321Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps3469467UNINA