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A A 402: Fluid Mechanics
3.00 Credits
University of Washington-Seattle Campus
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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A A 402 - Fluid Mechanics
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A A 405: Introduction to Aerospace Plasmas
3.00 Credits
University of Washington-Seattle Campus
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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A A 405 - Introduction to Aerospace Plasmas
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A A 406: PLASMA PROC GAS DCH
3.00 Credits
University of Washington-Seattle Campus
No course description available.
Prerequisite:
Separate File
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A A 406 - PLASMA PROC GAS DCH
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A A 409: Computer Tools for Aerospace III
2.00 Credits
University of Washington-Seattle Campus
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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A A 409 - Computer Tools for Aerospace III
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A A 410: Aircraft Design I
4.00 Credits
University of Washington-Seattle Campus
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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A A 410 - Aircraft Design I
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A A 411: Aircraft Design II
4.00 Credits
University of Washington-Seattle Campus
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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A A 411 - Aircraft Design II
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A A 412: AEROSP STRUC DESIGN
3.00 Credits
University of Washington-Seattle Campus
No course description available.
Prerequisite:
Separate File
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A A 412 - AEROSP STRUC DESIGN
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A A 419: Aerospace Heat Transfer
3.00 Credits
University of Washington-Seattle Campus
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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A A 419 - Aerospace Heat Transfer
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A A 420: Spacecraft and Space Systems Design I
4.00 Credits
University of Washington-Seattle Campus
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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A A 421: Spacecraft and Space System Design II
4.00 Credits
University of Washington-Seattle Campus
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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A A 421 - Spacecraft and Space System Design II
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