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Course Criteria
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3.00 Credits
Inviscid equations of motion, incompressible potential flows, small perturbation flows, bodies of revolution, viscous equations, exact solutions, laminar boundarylayer equations, similar solutions, integral methods. Compressibility, instability, turbulent boundary layers. Offered: Sp.
Prerequisite:
MATH 324; A A 301
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3.00 Credits
Development of introductory e romagnetic theory including Lorentz force and Maxwell’s equations. Plasma description. Single particle motions and drifts in magnetic and electric fields. Derivation of plasma fluid model. Introduction to plasma waves. Applications to electric propulsion, magnetic confinement, and plasmas in space and Earth’s outer atmosphere. Offered: A.
Prerequisite:
PHYS 123; MATH 324
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3.00 Credits
No course description available.
Prerequisite:
Separate File
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2.00 Credits
Computer-aided drawing basics, threedimensional drawing, projections, views. Computer-aided design and analysis tools for stress and heat transfer calculations. Offered: A.
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4.00 Credits
Conceptual design of a modern airplane to satisfy a given set of requirements. Estimation of size, se ion of configuration, weight and balance, and performance. Satisfaction of stability, control, and handling qualities requirements. Offered: W.
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4.00 Credits
Preliminary design of a modern airplane to satisfy a given set of requirements. Estimation of size, se ion of configuration, weight and balance, and performance. Satisfaction of stability, control, and handling qualities requirements. Offered: Sp.
Prerequisite:
A A 410
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3.00 Credits
No course description available.
Prerequisite:
Separate File
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3.00 Credits
Fundamentals of conductive, convective, and radiative heat transfer with emphasis on applications to atmospheric and space flight. Offered: W.
Prerequisite:
PHYS 123; MATH 307
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4.00 Credits
Design of space systems and spacecraft for advanced near-Earth and interplanetary missions. Astrodynamics, space environment, space systems engineering. Mission design and analysis, space vehicle propulsion, flight mechanics, atmospheric entry, aerobraking, configuration, structural design, power systems. thermal management, systems integration. Oral presentations and report writing. Design topics vary. Offered: W.
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4.00 Credits
A continuation of 420. Course content varies from year to year and is dependent on the design topic chosen for 420. Offered: Sp.
Prerequisite:
A A 420
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