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Course Criteria
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3.00 Credits
Same as Engineering Mechanics 339. Curved beams, shear deformation, beam columns, beams on elastic foundations; inelastic behavior of members; elementary plate bending. Three lecture hours a week for one semester. Prerequisite: Engineering Mechanics 319 with a grade of at least C-.
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3.00 Credits
Navier-Stokes equations, laminar and turbulent boundary layers, transition, effects of pressure gradients and compressibility. Three lecture hours a week for one semester. Prerequisite: Aerospace Engineering 320 with a grade of at least C-.
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3.00 Credits
Development and implementation of finite-difference schemes for numerical solution of subsonic, transonic, and supersonic flows. Emphasis on convection and diffusion equations of fluid dynamics. Evaluation of accuracy, stability, and efficiency. Three lecture hours a week for one semester. Aerospace Engineering 347 and Mechanical Engineering 369L may not both be counted. Prerequisite: Aerospace Engineering 311 and 320 with a grade of at least C- in each.
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3.00 Credits
Studies static aeroelastic phenomena; wing torsional divergence, control reversal, effect of wing sweep, flexibility effects on aircraft stability and control, and design implications; dynamic aeroelasticity; and galloping of transmission lines, flutter, and unsteady aerodynamics. Includes an introduction to experimental aeroelasticity. Three lecture hours a week for one semester. Prerequisite: Aerospace Engineering 321K and 330M with a grade of at least C- in each.
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3.00 Credits
Anisotropic constitutive relationships, lamination theory, failure theories, micromechanical behavior of laminates; laminated composite plates--bending, vibration, and buckling; composite fabrication, sandwich and other composite lightweight structures. Three lecture hours a week for one semester. Prerequisite: Aerospace Engineering 321K with a grade of at least C-.
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3.00 Credits
Conceptual design of an aircraft to meet a mission specification. Includes estimation of weight, cost from payload, and range requirements; selection of configuration; preliminary sizing of wing, fuselage, and tail/canard; aerodynamic design of wing and tail; weight and balance; and performance estimation. Three lecture hours and four laboratory hours a week for one semester. Prerequisite: Aerospace Engineering 367K with a grade of at least C-, and credit with a grade of at least C- or registration for Aerospace Engineering 364 and 376K.
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3.00 Credits
Preliminary design of an aircraft from a conceptual design to satisfy a given set of requirements. Includes preliminary structural design; detailed estimates of weight, balance, and performance; and satisfaction of stability, control, and handling quality requirements. Three lecture hours and four laboratory hours a week for one semester. Prerequisite: Aerospace Engineering 321K and 361K with a grade of at least C- in each, and credit with a grade of at least C- or registration for Aerospace Engineering 324L and 370L.
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3.00 Credits
Shock and expansion waves, quasi-one-dimensional flow, convergingdiverging nozzles, diffusers, wind tunnel operation, linearized flow, and compressibility effects on aerodynamics of airfoils and bodies. Three lecture hours a week for one semester. Prerequisite: Aerospace Engineering 320 with a grade of at least C-.
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3.00 Credits
History and principles of space flight from early Chinese rocket experiments to Apollo 17 and the Space Shuttle; technological benefits from the space program and future space projects. Three lecture hours a week for one semester. May not be counted as an aerospace engineering course for the Bachelor of Science in Aerospace Engineering; may not be counted as a technical elective, a technical area course, or an engineering elective for any engineering degree. Prerequisite: Upper-division standing or consent of instructor.
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3.00 Credits
Detailed analysis of aerodynamics of compressible and incompressible flows about wings and airfoils; wing and airfoil parameters and force and moment coefficients; and thin-airfoil theory, lifting-line theory, panel methods, high-lift devices, delta wings, transonic flows, and supersonic flows over wings. Three lecture hours a week for one semester. Aerospace Engineering 364 and 379L (Topic: Airfoil and Wing Design Theory) may not both be counted. Prerequisite: Aerospace Engineering 362K with a grade of at least C-, and credit with a grade of at least C- or registration for Aerospace Engineering 162M.
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