|
|
|
|
|
|
|
|
|
|
Course Criteria
Add courses to your favorites to save, share, and find your best transfer school.
-
0.00 - 3.00 Credits
3 hours. Prerequisites: AEM 249 and AEM 250. Methods of analyzing stressed skin structures of the types that are typically found in aircraft, missiles, and space vehicles. Unsymmetrical bending and bending and twisting of multiple cell structures are also covered.
-
0.00 - 3.00 Credits
3 hours. Prerequisites: AEM 249. Elements of statistics, matrix algebra, numerical analysis, and partial differential equations applied to engineering problems. Includes extensive computer applications.
-
1.00 - 3.00 Credits
3 hours. Prerequisites: AEM 314 and MATH 238. Corequisite: AEM 349 or MATH 237. Fundamentals of airplane flight dynamics, static trim, and stability.
-
2.00 - 3.00 Credits
3 hours. Prerequisites: AEM 413, AEM 341, and AEM 368. Corequisite: AEM 408. Preliminary design techniques for an aerospace system.
-
1.00 - 6.00 Credits
3 hours. Prerequisite: AEM 402. Preliminary and detailed design of aircraft and space vehicles, including weight and balance, power plant selection, exterior layout, performance, stability, and control. Involves group efforts on selected projects.
-
0.00 - 3.00 Credits
3 hours. Prerequisite: AEM 413. Basic propulsion dynamics, thermodynamics of fluid flow, combustion kinetics, air-breathing engines, rockets, design criteria, performance, and advanced propulsion systems.
-
3.00 Credits
3 hours. Prerequisites: AEM 313 and ME 215. Dynamics of compressible fluids: shock waves, one-dimensional flow, expansion waves in two-dimensional flow, and compressible flow over aerodynamic bodies.
-
0.00 - 3.00 Credits
3 hours. Prerequisite: AEM 313. Critical examination of the propulsive airscrew, including induced velocity relations, flow patterns, and similarity. Practical applications are approached through existing theory and practice.
-
0.00 - 3.00 Credits
3 hours. Prerequisite: AEM 468. This course introduces the student to the theory and practice of spacecraft dynamics and control. The topics covered include kinematics and dynamics of angular motion, spacecraft stabilization, attitude control devices, and design of linear and nonlinear spacecraft control systems.
-
0.00 - 3.00 Credits
3 hours. Prerequisite: AEM 408. This course introduces the student to descriptions and analyses of space and launch-vehicle propulsion. Topics covered include advanced schemes such as nuclear, solar, and laser propulsion; power cycles; and tether systems.
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Privacy Statement
|
Terms of Use
|
Institutional Membership Information
|
About AcademyOne
Copyright 2006 - 2025 AcademyOne, Inc.
|
|
|