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Course Criteria
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3.00 Credits
Convective heat transfer and viscous drag in high- temperature and high-speed flowfields. Inviscid hypersonic theory, real gas effects, and wall thermal protection strategies.
Prerequisite:
Undergraduate Semester level AE 3021 Minimum Grade of D
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3.00 Credits
Introduction to composite systems. Principles of manufacturing, structural mechanics of laminated composites. Aerospace design applications. Damage tolerance.
Prerequisite:
Undergraduate Semester level COE 2001 Minimum Grade of D
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0.00 - 3.00 Credits
Finite Element Method and its application to linear structural problems. The basic formulations of various structural elements are discussed.
Prerequisite:
Undergraduate Semester level AE 3125 Minimum Grade of D
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3.00 Credits
Multiaxial stress states, inelasticity in metals and polymers, yield criteria, metal fatigue, fracture, stress intensity factors, fracture toughness, fatigue crack growth, metal creep, and polymer viscoelasticity.
Prerequisite:
Undergraduate Semester level COE 3001 Minimum Grade of D
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3.00 Credits
Structural dynamics of one-dimensional systems. Analysis of static aeroelastic phenomena, unsteady aerodynamics, and flutter. Equations of motion for complete aeroelastic systems; solution techniques.
Prerequisite:
Undergraduate Semester level AE 3125 Minimum Grade of D and Undergraduate Semester level AE 3515 Minimum Grade of D
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3.00 Credits
First course in astrodynamics that encompasses two-body orbital mechanics, orbit determination, orbital maneuvers, orbital prediction, interplanetary trajectories, launch and space vehicle performance and atmospheric entry. Students cannot receive credit for both AE 4310 and AE 4532.
Prerequisite:
Undergraduate Semester level AE 2220 Minimum Grade of D
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0.00 - 3.00 Credits
Aircraft Vehicle Design. Preliminary design or case study of a complete flight vehicle, including a propulsion system, a structural system, and a control system. Students cannot receive credit for both AE 4341 and AE 4350.
Prerequisite:
Undergraduate Semester level AE 3330 Minimum Grade of D and Undergraduate Semester level AE 3340 Minimum Grade of D
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0.00 - 3.00 Credits
Spacecraft subsystems and synthesis. Students apply mission and spacecraft design principles in developing a space flight mission concept. Topics may vary. Students cannot receive credit for AE 4342 and AE 4356.
Prerequisite:
Undergraduate Semester level AE 3330 Minimum Grade of D and Undergraduate Semester level AE 3340 Minimum Grade of D
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0.00 - 3.00 Credits
Rotorcraft Vehicle Design. Preliminary design or case study of a complete rotorcraft flight vehicle, including a propulsion system, a structural system, and a control system. Students cannot receive credit for both AE 4343 and AE 4358 or AE 4343 and AE 6333.
Prerequisite:
Undergraduate Semester level AE 3330 Minimum Grade of D and Undergraduate Semester level AE 3340 Minimum Grade of D
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0.00 - 3.00 Credits
Conceptual design methodology developed and applied incorporating center of gravity, inertias, structural layout, materials, propulsion integration, stability and control, vehicle sizing, performance, and acquisition costs. Students cannot receive credit for both AE 4350 and AE 4341.
Prerequisite:
Undergraduate Semester level AE 3021 Minimum Grade of D and Undergraduate Semester level AE 3310 Minimum Grade of D and Undergraduate Semester level AE 3521 Minimum Grade of D and Undergraduate Semester level AE 4451 Minimum Grade of D
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