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Nov 21, 2024
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ME 882 - Compressible Flow3 lecture hours 0 lab hours 3 credits Course Description This course covers one-dimensional gas dynamics; shocks and waves, two-dimensional flows, perturbation theory; similarity rules, effects of viscosity and conductivity. The course culminates in a computer project in which a supersonic nozzle will be designed using the method of characteristics. (prereq: graduate standing and ME-317 or equivalent) Course Learning Outcomes Upon successful completion of this course, the student will be able to: • Apply engineering principles and analyze problems dealing with compressible flow and gas dynamics • Compare shock expansion with linearized theory for subsonic and supersonic flow over airfoils • Design a supersonic nozzle using the method of characteristics Prerequisites by Topic • Fluid mechanics • Thermodynamics (covering II Law) Course Topics • Review of the fundamentals (Laws of Thermodynamics, Conservation of Mass, Momentum and Energy, Entropy changes for perfect gases, Stagnation properties) • Introduction to Compressible Flow (Sonic velocity, Mach number, Stagnation relations in terms of Mach number, total pressure loss and entropy change relation, isentropic flow tables) • Standing Normal Shocks • Fanno Flow and applications • Rayleigh Flow and applications • Oblique Shocks • Prandtl-Meyer Flow (including lift and drag calculations on airfoils at various angles of attack) • Varying-Area Adiabatic flow (convergent-divergent nozzle, diffuser, choking) • Supersonic Nozzle Experiment and Mach number calculations • Topic: Applications of Compressible Flow in Propulsion Systems (Example: ramjet engine) • Differential Conservation Equations • Moving Normal Shock Waves • Velocity Potential Equation • Linearized Flow: subsonic and supersonic • Conical Flow • Method of Characteristics • Finite difference techniques for steady supersonic flow Laboratory Topics • Supersonic Nozzle experiment Coordinator Subha Kumpaty
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