|
|
|
|
|
|
|
|
|
|
Course Criteria
Add courses to your favorites to save, share, and find your best transfer school.
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
-
3.00 Credits
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
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Privacy Statement
|
Terms of Use
|
Institutional Membership Information
|
About AcademyOne
Copyright 2006 - 2025 AcademyOne, Inc.
|
|
|