01896oam 2200529 450 991071404870332120201113143306.0(CKB)5470000002507160(OCoLC)1136490319(EXLCZ)99547000000250716020200116d1930 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSpan load distribution on two monoplane wing models as affected by twist and sweepback /by Montgomery Knight and Richard W. NoyesWashington, [D.C.] :National Advisory Committee for Aeronautics,1930.1 online resource (7 pages, 12 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 346"July, 1930."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).AirplanesModelsWingsLoads (Mechanics)Stability of airplanesAirplanesModelsWingsfastLoads (Mechanics)fastStability of airplanesfastAirplanesModelsWings.Loads (Mechanics)Stability of airplanes.AirplanesModelsWings.Loads (Mechanics)Stability of airplanes.Knight Montgomery1390967Noyes Richard W.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910714048703321Span load distribution on two monoplane wing models as affected by twist and sweepback3487447UNINA