Aerodynamics of Propulsion

aerodynamic air intake aircraft annular airfoil area ratio available energy axial axial compressors axis boundary layer burner calculation Carnot cycle coefficient combustion chamber complex potential compression compressor const constant cooler block critical Mach cross section curve cylinder diffuser ducted propeller enthalpy entropy equation exit fairing flight speed free stream frontal area fuel fuselage given by Eq heat exchangers hodograph increase inflow losses integration interference drag isentropic jet engines kinetic energy mass flow maximum mechanical energy momentum theorem NACA nacelle nonducted nose nozzle obtained optimum outer surface over-all parallel flow plane potential flow pressure distribution pressure drop problems radius ram jet reduced shape shown in Fig stream function streamline subsonic supersonic T₁ temperature thermal efficiency thermodynamic thrust force tion turbine turbojet turbojet engine two-dimensional V₁ velocity components velocity increment vortex distribution vortex ring vortices wall wing Ро