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Fundamentals of rocket and airbreathing jet propulsion devices; prediction of thrust, combustion reactions, specific fuel consumption, and operating performance; ramjets; turbojets; turbofans; turboprops; aerothermodynamics of inlets, combustors, and nozzles; compressors, turbines; component matching. 3 undergraduate hours. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
Basic principles of chemical rocket propulsion and performance, rocket component design, liquid rockets, solid rocket motors, combustion processes, combustion instability. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
Elements of electric propulsion as applied to near-earth and deep-space missions; impact on spacecraft design; physics of ionized gases; plasmadynamics; electrothermal, electromagnetic, and electrostatic acceleration of gases to high velocity; high-impulse thruster design and performance; the resistojet, arcjet, ion engine, Hall thruster, MPD arc thruster, and plasma gun. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite:
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Introduction to the design of aerospace flight systems. Principles of systems engineering as they apply to the design process; general design methodology; application of these concepts to the initial sizing of both aircraft and spacecraft systems. Involves intensive technical writing. Involves intensive technical writing.
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Continuation of
Score: 4.8840237 Details | Listing | Web page
Advanced fundamental treatment of aerodynamic and dynamic structural phenomena associated with flexible airplanes and missiles; divergence of linear and nonlinear elastic lifting surfaces; effect of elastic and inelastic deformations on lift distributions and stability; elastic flutter of straight and swept wings; equations of disturbed motion of elastic and inelastic aircraft; dynamic response to forces, gusts, and continuous atmospheric turbulence; creep divergence of lifting surfaces; flutter in the presence of creep; effect of temperature on inelastic divergence and flutter. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite:
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Examines the common core of dynamics and control theory. Fundamental concepts of Lagrangian dynamics, state space representations, Hamiltonian and modern dynamics, stability theory, and control of dynamical systems. 3 undergraduate hours. 4 graduate hours. Prerequisite:
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Examines theory and application of experimental techniques in aerospace engineering with emphasis on fluid dynamic, aerodynamic, thermal, combustion, and propulsion phenomena. 2 undergraduate hours. No graduate credit. Prerequisite:
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Score: 4.8840237 Details | Listing | Web page
Introduction to numerical methods used in aerospace engineering. Finite difference method; Variational principles and Rayleigh-Ritz method; finite element method; applications from simple structural mechanics and aerodynamics problems encountered in aerospace engineering. 3 undergraduate hours. No graduate credit. Prerequisite:
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Aerodynamic, electromechanical, and structural design of wind power systems; classical windmills; modern wind power generators; wind characteristics and distribution; instrumentation and measurement; energy storage considerations; socioeconomics of wind power systems; performance of large and small scale wind turbines; current design approaches. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: A fluids course, an electrical course, and a course in mechanics, all at the 200 level or higher.
Score: 4.8840237 Details | Listing | Web page
Same as
Score: 4.8840237 Details | Listing | Web page
Independent theoretical and experimental projects in aerospace engineering. May be repeated. Prerequisite: Consent of instructor.
Score: 4.8840237 Details | Listing | Web page
Subject offerings of new and developing areas of knowledge in aerospace engineering intended to augment the existing curriculum. See Class Schedule or department course information for topics and prerequisite. May be repeated in the same or separate terms if topics vary to a maximum of 9 undergraduate hours or 12 graduate hours.
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Circular restricted three body problem; surfaces of zero velocity, libration points, and halo orbits; perturbed two body motion; Gauss and Lagrange planetary equations, Hamilton's principle, canonical equations and Delaunay variables; application to artificial Earth satellites; orbit determination. Prerequisite:
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Formulation of parameter and functional optimization problems for dynamic systems; applications of optimization principles to the control and performance of aerospace vehicles, including optimal flight paths, trajectories, and feedback control. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
Optimal rocket trajectories in inverse-square and linearized gravitational fields; orbital transfer, intercept, and rendezvous; high-thrust (impulsive) and low-thrust (continuous) trajectories; primer vector theory and applications; cooperative rendezvous. Prerequisite: Credit or concurrent registration in
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Same as
Score: 4.8840237 Details | Listing | Web page
Fundamentals of transonic flows; transonic characteristics and flow modeling, shock wave development, properties of shock wave, transonic similarity, shock-boundary layer interactions, three-dimensional effects, transonic solution techniques, transonic design, and transonic testing. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
Basic overview of the physics, governing equations and numerical methods for dispersed multiphase flow (also sometimes called particle suspensions), with particular emphasis on themomentum transfer to and from the particles. Characterization of particle size, shape, trajectories and coupling regimes; mixed-fluid, separated-fluid, and resolved-surface numerical approaches. Prerequisite:
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Boundary layer concept at high Reynolds numbers; self-similar solutions of incompressible and compressible boundary layers; stability of parallel and nearly-parallel wall-bounded viscous flows; transition to turbulence; turbulent boundary layers; high-speed boundary layers; strong Reynolds analogy; Morkovin's hypothesis. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
Theoretical analysis of the aerodynamic characteristics of two- and three-dimensional wings and multiple-body systems in subsonic and supersonic flows. Prerequisite: AE 413 or
Score: 4.8840237 Details | Listing | Web page
Importance and historical development of stress waves in solids; one-dimensional stress waves; three-dimensional longitudinal and shear waves, reflection and refraction of plane waves; Rayleigh and Love waves; wave guides; spherical waves, inelastic wave propagation and shock waves; dynamic fracture and shear bandings of solids; wave propagation in anisotropic media; experimental techniques; acoustic emission, ultrasounds, split Hopkinson (Kolsky) bar, plate impact experiments, optical techniques in dynamic fracture, high-speed photography. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
Short- and long-range dipole and electronic interactions; particle- and surface-force interactions; contact mechanics of rigid and nonrigid media, continuum adhesion models; principles of Atomic Force Microscopy (AFM), artifacts and remedies in AFM imaging; force and scale calibration; dynamics of AC-AFM imaging; force spectroscopy, instrumented nanoindentation. Prerequisite:
Score: 4.8840237 Details | Listing | Web page
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