01885oam 2200529I 450 991071381890332120200915143446.0(CKB)5470000002505467(OCoLC)1136490256(EXLCZ)99547000000250546720200116d1929 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind tunnel pressure distribution tests on an airfoil with trailing edge flap /by Carl J. Wenzinger and Oscar Loeser, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1929.1 online resource (10 pages, 12 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 326"October, 1929."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 7-8).AerofoilsFlaps (Airplanes)Wind tunnel testingAerodynamic loadTestingAerodynamic loadTestingfastWind tunnel testingfastAerofoils.Flaps (Airplanes)Wind tunnel testing.Aerodynamic loadTesting.Aerodynamic loadTesting.Wind tunnel testing.Wenzinger Carl J(Carl Joseph),1903-1988,1386955Loeser OscarJr.,United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713818903321Wind tunnel pressure distribution tests on an airfoil with trailing edge flap3487002UNINA