01788oam 2200493 450 991071602130332120210528125959.0(CKB)5470000002517895(OCoLC)1150919730(EXLCZ)99547000000251789520200416d1936 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y /by H.A. PearsonWashington, [D.C.] :National Advisory Committee for Aeronautics,1936.1 online resource (19 pages, 12 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 571"June 1936."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 18).AerofoilsSplit flaps (Airplanes)AerodynamicsForecastingAerofoilsfastSplit flaps (Airplanes)fastAerofoils.Split flaps (Airplanes)AerodynamicsForecasting.Aerofoils.Split flaps (Airplanes)Pearson Henry A(Henry Adolph),1906-1398867United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716021303321A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y3463074UNINA