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Course Criteria
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3.00 Credits
Static and vibratory response of framed structures. The matrix eigenvalue problem for buckling and free vibrations. Static response of laminated composite plates by the finite element method. Pre: 3124 or 3224. (3H,3 Credits).
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3.00 Credits
Introduction to the methods of static structural stability analysis and their applications. Buckling of columns and frames. Energy method and approximate solutions. Elastic and inelastic behavior. Torsional and lateral buckling. Use of stability as a structural design criterion. II. Pre: 3024, CEE 3404. (3H,3 Credits).
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3.00 Credits
Course designed to build upon and broaden a basic traditional engineering knowledge of fluid flows into areas concerning a variety of natural occurrences and phenomena that involve fluid motions in important ways. Drag of sessil systems and motile animals, gliding and soaring, flying and swimming, internal flows in organisms, low Reynolds number flows, fluid-fluid interfaces, unsteady flows in nature and wind engineering. Pre: 3014 or CEE 3304 or ESM 3024 or ME 3404. (3H,3 Credits). I.
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3.00 Credits
Analysis and design of various space, aeronautical and marine vehicles and systems. Senior standing required. (2H,3L,3 Credits).
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3.00 Credits
Use of mathematical programming methods for engineering design optimization including linear programming, penalty function methods, and gradient projection methods. Applications to minimum weight design, open-loop optimum control, machine design, and appropriate design problems from other engineering disciplines. Pre: MATH 2224. (3H,3 Credits).
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3.00 Credits
Development of computational methods for application to wing aerodynamic problems. Incompressible airfoil codes. Panel methods and vortex lattice methods. Finite difference techniques. Transonic and supersonic applications. Pre: 3044, 3114. (3H,3 Credits).
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3.00 Credits
Aerodynamic design of flight vehicles, with emphasis on nonlinear flowfields and configuration concepts. Aerodynamic analysis and design for transonic, supersonic, hypersonic flows, and low speed high alpha flight. Includes case studies of classic configurations and aerodynamic design papers. Pre: 3014, 3114. (3H,3 Credits).
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3.00 Credits
Application of Newton's Laws to the dynamics of spaceflight. Two-body problem, Kepler's Laws, energy and time relations, orbit specification and determination. Orbital maneuver and transfer, patched conic approximations, relative motion, and elements of optimal maneuvering. Must have a C- or better in prerequisite ESM 2304. Pre: ESM 2304. (3H,3 Credits).
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3.00 Credits
Space missions and the way pointing requirements affect attitude control systems. Rotational kinematics and attitude determination algorithms. Modeling and analysis of the attitude dynamics of space vehicles. Rigid body dynamics, effects of energy dissipation. Gravity gradient, spin, and dual spin stabilization. Rotational maneuvers. Environmental torques. Impacts of attitude stabilization techniques on mission performance. Must have a C- or better in pre-requisites AOE 3034 and 4134. Pre: 3034, 4134. (3H,3 Credits).
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3.00 Credits
Introduction and history of aircraft automatic flight control. Mathematical models of linear systems elements. Bode amplitude and phase plots of longitudinal and lateral control system analysis. Inputs and system performance assessment. Multiloop flight control systems. Applications to representative aircraft. Pre: 3134, MATH 4564. (3H,3 Credits).
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