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Course Criteria
Add courses to your favorites to save, share, and find your best transfer school.
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1.00 - 10.00 Credits
FLD. SU. Pr., departmental approval. Course may be repeated for a maximum of 10 credit hours.
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1.00 - 10.00 Credits
DSR. TD. Pr., departmental approval. Individualized support and direction for students writing their dissertation. Course may be repeated for a maximum of 10 hours.
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2.00 Credits
LEC. 1, LAB. 3. Pr., ENGR 1110. Introduction to the fundamental physical concepts required for the successful design of aircraft and spacecraft.
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3.00 Credits
LEC. 3. Pr., sophomore standing. Basic principles, causes, effects, and phenomena of weather with fundamental techniques of forecasting.
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3.00 Credits
LEC. 3. Pr., MATH 2650. Properties of fluids, fluid statics, conservation of mass and momentum, atmospheric properties, two dimensional airfoils, three dimensional wings, drag, and flight performance.
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3.00 Credits
LEC. 3. Pr., AERO 3110, ENGR 2010. Principles of compressible flow including flows with area changes, friction and heat transfer. Fundamental analysis of aerodynamics and potential flow theory. Correlation of potential flow theory with experimental data.
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2.00 Credits
LEC. 1, LAB. 3. Pr., AERO 3110. Application of fundamental aerodynamic principles to subsonic and supersonic wind tunnel experiments.
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3.00 Credits
LEC. 3. Pr., ENGR 2350, MATH 2650. Modeling of system elements, classical feedback control techniques used in the analysis of linear systems, analysis of systems undergoing various motions connected with flight.
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4.00 Credits
LEC. 3, LAB. 3. Pr., AERO 3110, ENGR 2350, MATH 2650. Airplane performance and stability and control including analytical prediction of performance characteristics, experimental determination of static stability parameters, and analytical prediction of dynamic stability characteristics.
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3.00 Credits
LEC. 3. Pr., ENGR 2350, MATH 2650. Geometry of the solar system and orbital motion, mathematical integrals of motion, detailed analysis of two-body dynamics and introduction to artificial satellite orbits; Hohmann transfer and patched conics for lunar and interplanetary trajectories.
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