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AE 397: Independent Study
1.00 - 3.00 Credits
University of Illinois at Urbana-Champaign
Independent theoretical and experimental projects in aerospace engineering. May be repeated. Prerequisite: Consent of instructor.
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AE 397 - Independent Study
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AE 402: Orbital Mechanics
3.00 - 4.00 Credits
University of Illinois at Urbana-Champaign
Analysis of orbits in an inverse-square gravitational field; elementary rocket dynamics, impulsive orbit transfer and rendezvous, and Lambert's Theorem with applications; patched-conic trajectories, planetary gravity-assist maneuvers, and linearized orbit theory with application to simplified analytical models; perturbations. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 202.
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AE 402 - Orbital Mechanics
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AE 403: Spacecraft Attitude Control
3.00 - 4.00 Credits
University of Illinois at Urbana-Champaign
Theory and applications of spacecraft attitude dynamics and control; Euler angles, direction cosines, quaternions, and Gibbs-Rodrigues parameters; attitude sensors and control actuators; spin, three-axis active, reaction wheel, control moment gyro, and gravity gradient control systems; environmental effects. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 352 and AE 353.
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AE 403 - Spacecraft Attitude Control
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AE 410: Computational Aerodynamics
3.00 - 4.00 Credits
University of Illinois at Urbana-Champaign
Computational technologies as solution tools for various aerodynamic problems; modeling and solution of one-and two-dimensional, incompressible and compressible, steady and unsteady inviscid external flow fields. Computational laboratory for practical experience. Same as CSE 461. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 311.
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AE 410 - Computational Aerodynamics
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AE 412: Viscous Flow & Heat Transfer
4.00 Credits
University of Illinois at Urbana-Champaign
Momentum and thermal transport in wall boundary-layer and free shear flows, solutions to the Navier-Stokes equations for heat conducting laminar and turbulent shear flows; similarity concepts; thermal boundary layers in ducts and high-speed aerodynamic boundary layers. Same as ME 411. Prerequisite: AE 311 or ME 310.
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AE 412 - Viscous Flow & Heat Transfer
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AE 416: Applied Aerodynamics
3.00 - 4.00 Credits
University of Illinois at Urbana-Champaign
Two-dimensional and finite wing theory with emphasis on the mechanisms of lift and drag generation; Reynolds number and Mach number effects; drag analysis; high-lift wing systems; propeller and rotor aerodynamics; control surface design; application of V/STOL aerodynamics. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 311.
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AE 416 - Applied Aerodynamics
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AE 419: Aircraft Flight Mechanics
3.00 - 4.00 Credits
University of Illinois at Urbana-Champaign
Steady and quasi-steady aircraft flight performance; take-off and landing, climbing and diving, cruise, level turn, and introduction to energy methods; longitudinal, directional, and lateral static stability and control; introduction to longitudinal and lateral motion and dynamic stability. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 202 and AE 353.
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AE 419 - Aircraft Flight Mechanics
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AE 420: Finite Element Analysis
3.00 - 4.00 Credits
University of Illinois at Urbana-Champaign
Same as CSE 451 and ME 471. See ME 471.
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AE 420 - Finite Element Analysis
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AE 427: Mechanics of Polymers
3.00 Credits
University of Illinois at Urbana-Champaign
Same as MSE 454 and TAM 427. See TAM 427.
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AE 427 - Mechanics of Polymers
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AE 428: Mechanics of Composites
3.00 Credits
University of Illinois at Urbana-Champaign
Same as MSE 456 and TAM 428. See TAM 428.
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AE 428 - Mechanics of Composites
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