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Course Criteria
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0.00 - 3.00 Credits
Cr. 3. Prereq : 351. An examination of spacecraft systems including attitude determination and control, power, thermal control, communications, propulsion, guidance, navigation, command and data handling, and mechanisms. Explanation of space and operational environments as they impact spacecraft design. Includes discussion of safety, reliability, quality, maintainability, testing, cost, legal, and logistics issues. Nonmajor graduate credit.
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1.00 - 6.00 Credits
Cr. 1-6. Repeatable. Prereq : Junior or senior classifi cation, approval of the department. A. Aero and/or Gas Dynamics B. Propulsion C. Aerospace Structures D. Flight Dynamics E. Spacecraft Systems F. Flight Control Systems G. Aeroelasticity H. Honors I. Design J. Non-destructive Evaluation K. Wind Engineering L. Multi-functional Ultra-light Structures O. Other
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3.00 Credits
Cr. R. F.S. (1-0) Professional skills development activities. Designed to encourage involvement in a variety of aerospace engineering activities and related professional activities. Engineering ethics case studies and discussions. Academic program planning, departmental symposium participation.
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3.00 Credits
Cr. R. F.S. (1-0) Professional skills development activities. Writing and presentation of a technical paper at the department's Aerospace Symposium or at a recognized student or professional meeting of the American Institute of Aeronautics and Astronautics (AIAA). Satisfactory-fail only.
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3.00 Credits
Cr. R. Repeatable. F.S.SS. Prereq: 398, permission of department and Engineering Career Services. Third and subsequent professional work periods in the cooperative education program. Students must register for this course before commencing work. Satisfactory-fail only.
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1.00 - 2.00 Credits
Cr. 1-2. Repeatable. F.S. Prereq: Senior classifi cation, credit or enrollment in 491. Development of aerospace principles and concepts through individual research and projects. Written report.
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0.00 - 3.00 Credits
(Cross-listed with E M). (3-0) Cr. 3. F. Prereq : E M 324. Theory of stress and strain, stress-strain relationships. Unsymmetrical bending, curved beams, shear center. Torsion of thin-walled noncircular sections. Equilibrium, compatibility equations. Airy stress functions. Membrane stresses in shells, thick-walled cylinders.
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2.00 - 3.00 Credits
(3-2) Cr. 4. Alt. S., offered 2008. Prereq : E M 510 or 514 or 516. Fundamental concepts for force, displacement, stress, and strain measurements. Strain gages. Full fi eld deformation measurements with laser interferometry and digital image processing. Advanced experimental concepts at the micro and nano scale regimes.
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0.00 - 3.00 Credits
Cr. 3. F. Prereq : 421 or E M 424. Analysis of static stresses and deformation in continuous aircraft structures. Various analytical and approximate methods of analysis of isotropic and anisotropic plates and shells.
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0.00 - 3.00 Credits
Cr. 3. Prereq : Math 385, profi ciency in programming. Introduction to modern mesh generation techniques. Structured and unstructured mesh methods, algebraic and PDE methods, elliptic and hyperbolic methods, variational methods, error analysis, Delaunay triangulation, data structures, geometric modeling with B-spline and NURBS surfaces, surface meshing.
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