02064oam 2200577 450 991071308290332120200316140507.0(CKB)5470000002499371(OCoLC)1107323816(EXLCZ)99547000000249937120190703d1921 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffects of varying the relative vertical position of wing and fuselage /by L. Prandtl[Washington, D.C.] :National Advisory Committee for Aeronautics,1921.1 online resource (4 pages, 6 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 75"December, 1921.""Extract from the First Report of the Gőttingen Aerodynamic Laboratory, Chap. IV, Sec. 7, pp. 118-120"--Page 1."Translated by the National Advisory Committee for Aeronautics"--Page 2.No Federal Depository Library Program (FDLP) item number.AirplanesWingsAirplanesFuselageAerodynamicsMechanical efficiencyAerodynamicsfastAirplanesFuselagefastAirplanesWingsfastMechanical efficiencyfastAirplanesWings.AirplanesFuselage.Aerodynamics.Mechanical efficiency.Aerodynamics.AirplanesFuselage.AirplanesWings.Mechanical efficiency.Prandtl Ludwig1875-1953,3749United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713082903321Effects of varying the relative vertical position of wing and fuselage3531293UNINA