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Concepts from thermodynamics and fluid mechanics
Flow in a duct of variable crosssectional area
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adiabatic flow assumed back pressure characteristics choked compressible flow compression wave considered constant cross-sectional area continuity equation control surface control volume convergent convergent-divergent duct denotes density diameter disturbances duct of constant energy equation engine enthalpy entropy change exit plane Fanno curve FANNO FLOW flow with friction Fluid Mechanics fluid properties friction factor given heat addition heat transfer infinitesimal inlet kg/s kN/m left-running waves Mach number mass flow rate maximum momentum equation neglected normal shock nozzle one-dimensional flow open end perfect gas pipe piston pitot position diagram pressure ratio RAYLEIGH FLOW reference reservoir second law second throat shock wave shown in Fig simple wave solution sonic speed of sound stagnation pressure stagnation temperature static pressure steady flow subsonic flow supersonic flow throat area tube upstream velocity of sound wave front wave propagating