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AA 295: Aerospace Structures and Materials

Presentations by researchers and industry professionals in aerospace structures and materials. May be repeated for credit.
Terms: Spr | Units: 1 | Repeatable for credit
Instructors: Chang, F. (PI)

AA 300: Engineer Thesis

Thesis for degree of Engineer. Students register for section belonging to their thesis adviser.
Terms: Aut, Win, Spr, Sum | Units: 1-15 | Repeatable for credit

AA 301: Ph.D. Dissertation

Prerequisite: completion of Ph.D qualifying exams. Students register for section belonging to their thesis adviser. (Staff)
Terms: Aut, Win, Spr, Sum | Units: 1-15 | Repeatable for credit

AA 801: TGR Engineer Thesis

Engineer's thesis or non-doctoral work for a TGR student.
Terms: Aut, Win, Spr, Sum | Units: 0 | Repeatable for credit

AA 201B: Topics in Aeroacoustics

Acoustic equations for moving medium, simple sources, Kirchhoff formula, and multipole representation; radiation from moving sources; acoustic analogy approach to sound generation in compact flows; theories of Lighthill, Powell, and Mohring; acoustic radiation from moving surfaces; theories of Curl, Ffowcs Williams, and Hawkings; application of acoustic theories to the noise from propulsive jets, and airframe and rotor noise; computational methods for acoustics. Prerequisite: 201A or consent of instructor.

AA 206: Bio-Aerodynamics

Topics: flapping flight, low Reynolds number aerodynamics, wing design, flocks, swarms, and dynamic soaring. Readings from current and historical literature dealing with theoretical and observational studies. Applications in aircraft design, and simulation-based problem sets. Prerequisite: course in aerodynamics such as 100, 200A, or 241A.

AA 208: Aerodynamics of Aircraft Dynamic Response and Stability

Companion to 200A for those interested in control and guidance. Typical vehicles and the technical tradeoffs affecting their design. Equations of motion, stressing applications to dynamic performance, stability, and forced response. Forms and sources for the required aerodynamic data. Response to small disturbances and stability derivatives. Static stability and trim. Review of aerodynamic fundamentals, leading to airload predictions for wings, bodies, and complete aircraft. Paneling and other methods for derivative estimation. Natural motions of the aircraft, and the influence on them of various configuration parameters. Vehicle behavior in maneuvers of small and large amplitudes. Prerequisites: 200A, 210A, or equivalents (may be taken concurrently).

AA 211B: PHYS GAS DYN

| Repeatable 1 times (up to 60 units total)

AA 214A: Numerical Methods in Fluid Mechanics

Instructors: Pulliam, T. (PI)

AA 238: Human-Centered Design for Aerospace Engineers

The what, when, who, and how of human-centered design. Is it art, magic, science, or engineering? How to integrate human-centered processes into engineering design processes. Analysis of recent human-centered aeronautical and space systems to evaluate successes and limitations.
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