01771oam 2200517 450 991071673700332120210824141202.0(CKB)5470000002524807(OCoLC)1159597610(EXLCZ)99547000000252480720200623d1937 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEmpirical corrections to the span load distribution at the tip /by H.A. PearsonWashington, [D.C.] :National Advisory Committee for Aeronautics,1937.1 online resource (10 pages, 6 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 606"August 1937."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 9-10).AirplanesWingsAerodynamic loadMathematical modelsAerodynamic loadfastAirplanesWingsfastMathematical analysisfastAirplanesWings.Aerodynamic load.Mathematical models.Aerodynamic load.AirplanesWings.Mathematical analysis.Pearson Henry A(Henry Adolph),1906-1398867United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716737003321Empirical corrections to the span load distribution at the tip3483587UNINA