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Dec 13, 2025
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MEC 4872 - Compressible Flow3 lecture hours 0 lab hours 3 credits Course Description This course covers compressible flow aerodynamics; conservation of mass, momentum, and energy; one-dimensional and quasi-one-dimensional flow; oblique shock waves and Prandtl-Meyer expansion waves; unsteady wave motion. Application to nozzles, diffusers, supersonic airfoils, and shock tubes. (prereq: MEC 2110 , MEC 3120 ) (quarter system prereq: ME 3102, ME 3104) Course Learning Outcomes Upon successful completion of this course, the student will be able to:
- Describe qualitatively and mathematically the propagation of disturbances in compressible media
- Differentiate between different flow regimes and describe their characteristic physical features
- Qualitatively and quantitatively describe the variation of flow and thermodynamic properties for isentropic flow through variable area geometries
- Explain when flows will choke and the consequences of choked flow
- Explain the physical mechanisms driving the formation of shocks (normal and oblique) and Prandtl-Meyer expansion fans
- Use equations and tables to determine how flow and thermodynamics properties vary across shocks and expansion fans
- Analyze problems in which oblique shocks and expansion fans reflect from solid surfaces
- Describe the wave structures that occur on various solid surfaces in supersonic flows and compute the resulting lift and drag forces
- Analyze moving normal shock problems including situations in which reflections occur.
- Describe the purpose of a shock tube and analyze the internal flow field of a shock tube
- Analyze Fanno and Rayleigh flow problems
- Explain the physical nature of the method of characteristics and numerically implement the technique to solve for the flow field in steady 2D and/or 1D unsteady compressible flow fields
Prerequisites by Topic
- First and second laws of thermodynamics
- Control volume mass, momentum, energy and entropy analysis
- Energy and entropy properties of ideal gases
- Coding in MATLAB
Course Topics
- Review of the fundamentals (laws of thermodynamics, conservation of mass, momentum and energy, entropy changes for perfect gases)
- Introduction to compressible flow (sonic velocity, Mach number, stagnation relations in terms of Mach number, total pressure loss and entropy change relation)
- Varying-area adiabatic flow (convergent-divergent nozzle, diffuser, choking, isentropic flow tables)
- Standing normal shocks
- Moving and oblique (planar or conical) shocks
- Analysis of shock tubes
- Prandtl-Meyer flow (including lift and drag calculations on airfoils at various angles of attack, and discussion on over-expanded and under-expanded nozzles)
- Fanno flow and applications
- Rayleigh flow and applications
- Method of characteristics applied to 2D steady and/or 1D unsteady flows
Coordinator Dr. Prabhakar Venkateswaran
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