02076oam 2200577 450 991071389400332120200820113958.0(CKB)5470000002504750(OCoLC)1104148302(EXLCZ)99547000000250475020190610d1952 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAirfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range /by Dean R. ChapmanWashington, [D.C.] :National Advisory Committee for Aeronautics,1952.1 online resource (44 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 2787"September 17, 1952."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 24).Aerodynamic loadAerodynamics, SupersonicAerofoilsDrag (Aerodynamics)Aerodynamic loadfastAerodynamics, SupersonicfastAerofoilsfastDrag (Aerodynamics)fastAerodynamic load.Aerodynamics, Supersonic.Aerofoils.Drag (Aerodynamics)Aerodynamic load.Aerodynamics, Supersonic.Aerofoils.Drag (Aerodynamics)Chapman Dean R.1401174United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713894003321Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range3493800UNINA