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Course Criteria
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0.00 - 3.00 Credits
Cr. 3. Prereq : 321, Math 266 or 267. Single and multiple degree of freedom vibration. Free and forced vibration. Matrix methods. Modal analysis, static aeroeasticity- divergence, control surface reversal. Dynamic aeroelasticty-fl utter. Application of fi nite element technique (ANSYS) to aeroelasticity problems. Nonmajor graduate credit.
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2.00 Credits
Cr. 3. Prereq : E M 324; Mat E 272. Fabrication, testing and analysis of composite materials used in fl ight structures. Basic laminate theory of beams, plates and shells. Manufacturing and machining considerations of various types of composites. Testing of composites for material properties, strength and defects. Student projects required. Nonmajor graduate credit.
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1.00 - 6.00 Credits
Cr. 3. Prereq : E M 324. Detailed design and analysis of aerospace vehicle structures. Material selection, strength, durability and damage tolerance, and validation analysis. Design for manufacturability. Nonmajor graduate credit.
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0.00 - 3.00 Credits
Cr. 3. Prereq : 331. Aircraft lateral directional stability augmentation. Launch vehicle pitch control system design. Control of fl exible vehicles. Satellite attitude control. Flight control designs based on state-space methods. Introduction to sample-data systems. Nonmajor graduate credit.
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0.00 - 3.00 Credits
(3-0) Cr. 3. Prereq : 355. Introduction to the aerodynamics, performance, stability, control and critical maneuvering characteristics of V/STOL vehicles. Topics include hovercrafts, jet fl aps, ducted fans and thrust vectored engines. Nonmajor graduate credit.
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0.00 - 3.00 Credits
Cr. 3. Prereq : 343. Introduction to modern computational fl uid dynamics. Finite difference and fi nite volume methods. Explicit, implicit, and iterative techniques. Solutions of elliptic, parabolic, and hyperbolic equations. Emphasis on applications. Commercial software. Nonmajor graduate credit.
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0.00 - 3.00 Credits
(Cross-listed with M E). (3-0) Cr. 3. S. Prereq: M E 335 or equivalent. Applications of principles of fl uid mechanics and thermodynamics in performance analysis and design of turbomachines and related fl uid system components. Nonmajor graduate credit.
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0.00 - 3.00 Credits
Cr. 3. Prereq : 351. Simple orbit determination and prediction. Advanced orbit maneuvers, single-, double-, and triple-impulse; fi xed-impulse, fi nite-duration. 3-D rigid-body dynamics, Euler's equations, satelitte stabilization and attitude control. Earth gravity fi eld models and gravity harmonics, orbit perturbations, variational methods, relative orbital mechanics, Clohessy-Wiltshire equations. Nonmajor graduate credit.
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2.00 Credits
Cr. 3. F.S. Prereq: 361, 311, 321, 351, 355. Introduction to modern engineering design methodology. Computational constrained optimal design approach including selection of objective function, characterization of constraint system, materials and strength considerations, and sensitivity analyses. Nonmajor graduate credit.
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1.00 - 4.00 Credits
Cr. 3. F.S. Prereq: 461. Fundamental principles used in engineering design of aircraft, missile, and space systems. Preliminary design of aerospace vehicles.
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