02508oam 2200673I 450 991071381920332120200915142107.0(CKB)5470000002505464(OCoLC)1136490271(EXLCZ)99547000000250546420200116d1929 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind tunnel pressure distribution tests on a series of biplane wing modelsPart IIEffects of changes in decalage, dihedral, sweepback and overhang /by Montgomery Knight and Richard W. NoyesWashington, [D.C.] :National Advisory Committee for Aeronautics,1929.1 online resource (6 pages, 32 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 325"October, 1929."Includes errata.No Federal Depository Library Program (FDLP) item number.Includes bibliographical reference (page 6).Effects of changes in decalage, dihedral, sweepback and overhangAirplanesDihedral wingsAirplanesModelsTestingAirplanesWings, Swept-backAerodynamic loadTestingWind tunnel testingBiplanesAerodynamic loadTestingfastAirplanesDihedral wingsfastAirplanesModelsTestingfastAirplanesWings, Swept-backfastWind tunnel testingfastAirplanesDihedral wings.AirplanesModelsTesting.AirplanesWings, Swept-back.Aerodynamic loadTesting.Wind tunnel testing.Biplanes.Aerodynamic loadTesting.AirplanesDihedral wings.AirplanesModelsTesting.AirplanesWings, Swept-back.Wind tunnel testing.Knight Montgomery1390967Noyes Richard W.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713819203321Wind tunnel pressure distribution tests on a series of biplane wing models3444189UNINA