01811oam 2200529 450 991071376290332120200729135624.0(CKB)5470000002504054(OCoLC)1104148286(EXLCZ)99547000000250405420190610d1949 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds /by John R. SpreiterWashington, [D.C.] :National Advisory Committee for Aeronautics,1949.1 online resource (32 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 1897"June 1949."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 30).Aerodynamic loadAerodynamicsAirplanesWingsAerodynamic loadfastAerodynamicsfastAirplanesWingsfastAerodynamic load.Aerodynamics.AirplanesWings.Aerodynamic load.Aerodynamics.AirplanesWings.Spreiter John R.1389691United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713762903321Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds3462006UNINA