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Course Criteria
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1.00 - 6.00 Credits
Special projects agreed upon by student and instructor. Instructor consent required.
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1.00 - 6.00 Credits
Assigns a research problem on an individual basis. Instructor consent required.
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3.00 Credits
Introduces finite element methods used for solving linear problems in structural and continuum mechanics. Covers modeling, mathematical formulation, and computer implementation. Prereq., matrix algebra.
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3.00 Credits
Studies the rotational motion of spacecrafts, including attitude parameters and spacecraft torques. Applies Euler equations to the attitude motions of simple spacecrafts and their stability. Prereq., ASEN 3200 or equivalent.
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3.00 Credits
Applies fundamental concepts of continuum mechanics, theory of elasticity, and energy methods to the analysis of structures. Prereqs., APPM 2360 and ASEN 2001, 2003, and 3112, or equivalent. Similar to MCEN 5023.
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3.00 Credits
Chemical combustion calculations for multicomponent gases and application to air-breathing and rocket propulsion systems; performance criteria and scaling laws; introduction to chemical reaction rates; combustion instability and nozzle heat transfer; ion propulsion and mhd generators.Prereq., ASEN 4013 or instructor consent.
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3.00 Credits
Introduces the theory of linear systems, including vector spaces, linear equations, structure of linear operators, state space descriptions of dynamic systems, and state feedback control methods. Prereq., ASEN 3200.
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3.00 Credits
Familiarizes students with factors affecting living organisms in the reduced-gravity environment of space flight. Covers basic life support requirements, human physiological adaptations, and cellular-level gravity dependent processes with emphasis on technical writing and research proposal preparation. Prereq., graduate standing in engineering or instructor consent.
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3.00 Credits
Studies low Reynolds number flows, including incompressible and compressible laminar boundary layer theory; similarity theory; and separation, transition, and turbulent boundary layers. Prereq., ASEN 5051 or equivalent, or instructor consent.
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3.00 Credits
Applies concepts covered in undergraduate dynamics, structures, and mathematics to the dynamics of aerospace structural components, including methods of dynamic analysis, vibrational characteristics, vibration measurements, and dynamic stability. Prereqs., ASEN 5012, 5227, or equivalent. Recommended prereq., MATH 3130.
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