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AE 162: Aerodynamics
3.00 Credits
San Jose State University
Aerodynamic forces, moments. Flow similarity. Potential flow. Airfoils, wings in low-speed, high-speed flow. Boundary layers, skin friction drag. Flow measurement, visualization in subsonic and smoke tunnels. Prerequisite: M E 111. Corequisite: E N G R 100 W. Lecture 2 hours/lab 3 hours. 3 units
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AE 162 - Aerodynamics
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AE 164: Compressible Flow
3.00 Credits
San Jose State University
Normal shock waves, oblique shocks, expansion waves, nozzle flow, heat addition, friction, method of characteristics. Numerical methods. Shock tunnel experiment. Prerequisites: E N G R 100 W, M E 111, M E 113. Lecture 2 hours/lab 3 hours. Repeatable for credit 3 units
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AE 164 - Compressible Flow
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AE 165: Aerospace Flight Mechanics
3.00 Credits
San Jose State University
Trajectory dynamics of atmospheric flight (aircraft and missiles) and spaceflight (orbital mechanics). Influence of vehicle design on trajectory. Aircraft static performance, stability and control. Rocket launch and re-entry dynamics. Computer simulations. Prerequisite: M E 101. 3 units
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AE 165 - Aerospace Flight Mechanics
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AE 167: Aerospace Propulsion
3.00 Credits
San Jose State University
Theory, design and performance of turbojet derivative engines, ramjet and hybrid engines, solid and liquid propellant rocket engines. Applications to aircraft, missile, and spacecraft systems. Prerequisites: M E 111 and M E 113. 3 units
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AE 167 - Aerospace Propulsion
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AE 168: Aerospace Vehicle Dynamics and Control
3.00 Credits
San Jose State University
Aircraft/spacecraft dynamics, stability and control. Linearization and Euler transformations. Eigenvalues and eigenvectors. State space and transfer function analysis of dynamics of aerospace vehicles. Feedback control design and synthesis using advanced control techniques. Prerequisites: A E 140, A E 165. 3 units
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AE 168 - Aerospace Vehicle Dynamics and Control
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AE 169: Computational Fluid Dynamics
3.00 Credits
San Jose State University
Physical and mathematical foundations of computational fluid mechanics with emphasis on applications. Solution methods for model equations and the Euter and the Navier- Stokes equations. The finite volume formulation of the equations. Classification of partial differential equations and solution techniques. Truncation errors, stability. Prerequisite: A E 164. Lecture 2 hours/lab 3 hours. 3 units
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AE 169 - Computational Fluid Dynamics
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AE 171A: Aircraft Design I
3.00 Credits
San Jose State University
Conceptual and preliminary design of airplanes. Mission specification, figures of merrit, weight sizing, performance constraint analysis, configuration design, fuselage design, wing and high-lift system design, empennage design, landing gear design. Ethics, safety and liability issues. Prerequisites: M E 20, A E 162, A E 165, A E 114. Pre/ Corequisite: A E 167. Lab 9 hours. 3 units
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AE 171A - Aircraft Design I
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AE 171B: Aircraft Design II
3.00 Credits
San Jose State University
Preliminary and detail design of aircraft. Weight and balance analysis, stability and control analysis, drag polar estimation, resizing. Participation in professional society design/build/fly competitions. Ethics, safety and liability issues. Prerequisites: A E 171 A, A E 167. Pre/ Corequisite: A E 168. Lab 9 hours. 3 units
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AE 171B - Aircraft Design II
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AE 172A: Spacecraft Design I
3.00 Credits
San Jose State University
Team-based preliminary design of planetary probes, spacecraft or launch vehicle. Development of an initial vehicle concept and a complete numerical model of the mission. Ethics, safety, and liability issues. Prerequisites: M E 20, A E 162, A E 165, A E 114. Pre/ Corequisite: A E 110, A E 167 Lab 9 hours. 3 units
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AE 172A - Spacecraft Design I
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AE 172B: Spacecraft Design II
3.00 Credits
San Jose State University
Preliminary and detail design of spacecraft. Spacecraft construction, integration, and testing. Ethics, safety, and liability issues. Prerequisites: M E 172 A, A E 167, A E 110. Pre/ Corequisite: A E 168.9 hour Lab. 3 units
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AE 172B - Spacecraft Design II
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