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AERO 6340/6346: Satellite Application
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 3310 or departmental approval. Principles related to the application of satellites to remote sensing, telecommunications, navigation and trajectory determination. Principles of space policy applied to both the unmanned and manned space flight programs.
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AERO 6340/6346 - Satellite Application
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AERO 6520/6526: Rocket Propulsion
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 4510. Analysis of the thermodynamics, gas dynamics and design of liquid and solid propellant rocket engines.
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AERO 6520/6526 - Rocket Propulsion
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AERO 6530/6536: Space Propulsion
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 4510. Analysis of space propulsion systems. Dynamics of electromagnetic systems, ion engines, photon drives, laser propulsion.
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AERO 6530/6536 - Space Propulsion
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AERO 6620/6626: Dynamic Simulation
3.00 Credits
Auburn University
LEC. 3. Pr., ENGR 2350. Computer techniques applied to the analysis of aerospace engineering problems using the digital problem-oriented language, Advanced Continuous Simulation Language (ACSL).
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AERO 6620/6626 - Dynamic Simulation
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AERO 6630/6636: Aerospace Applications of Composite Materials
4.00 Credits
Auburn University
LEC. 3, LAB. 3. Pr., AERO 3610. Basic material and manufacturing information for laminated composite structures. Computational structural analysis of typical aerospace composite structures coupled with experimental verification of the structural response.
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AERO 6630/6636 - Aerospace Applications of Composite Materials
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AERO 6750/6756: Legal Aspects of Engineering Practice
3.00 Credits
Auburn University
LEC. 3. Pr., PHIL 1020. The role of the law in the manufacture of a product. Ethical issues that may confront designers and engineers.
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AERO 6750/6756 - Legal Aspects of Engineering Practice
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AERO 7100/7106: Adv Supersonic Aerodynamics
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 4140. A rigorous development of linearized and nonlinear fluid flow theories and application. Lifting surfaces, lifting bodies, duct flow, boundary layer effects, shock and expansion waves and method of characteristics.
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AERO 7100/7106 - Adv Supersonic Aerodynamics
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AERO 7110/7116: Airfoil Aerodynamics
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 3120. Thin airfoil theory, Joukowski transformations, Karman Trefftz transformations, thick airfoil theory, panel methods and comparison with experimental data.
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AERO 7110/7116 - Airfoil Aerodynamics
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AERO 7120/7126: Dynamics of Viscous Fluids I
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 7100. Exact solutions to the Navier Stokes equations. Exact and approximate solutions of the laminar boundary layer equations. Incompressible and compressible boundary layers in theory and experiment.
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AERO 7120/7126 - Dynamics of Viscous Fluids I
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AERO 7130/7136: Dynamics of Viscous Fluids II
3.00 Credits
Auburn University
LEC. 3. Pr., AERO 7120. Turbulent flows, the Reynolds stresses and turbulence modeling. Computation of incompressible and compressible turbulent boundary layers. Stability theory and transition.
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AERO 7130/7136 - Dynamics of Viscous Fluids II
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