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Course Criteria
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2.00 Credits
and complements material in courses on aerodynamics, structures and dynamics; basic testing techniques and use of computers. Prerequisite: ; AERO 301 or registration therein.
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3.00 Credits
of compressible flow, acoustic waves, shock and expansion waves, shock-expansion theory, supersonic airfoil design, small perturbation theory, conical flow theory, supersonic wing panel methods, supersonic wing design, similarity theory, cone flow, unsteady waves, and theory of characteristics. Prerequisites: AERO 1, 301.
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4.00 Credits
design considerations; mechanics of structures; introduction to elasticity; constitution of materials; analysis of typical aerospace structures in bending, extension, torsion and shear. Prerequisites: AERO 30 or registration therein; AERO 13, 14, MATH 308.
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2.00 Credits
Aerospace Engineering Laboratory II. (1-3). Credit 2. Demonstrates and complements material on aircraft stability and control and propulsion as well as aerodynamics and structures. Prerequisites: AERO 304, 310; ECEN 215.
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3.00 Credits
Aerospace Structural Analysis II. (3-0). Credit 3. Work and energy principles; analysis of indeterminate structures by classical virtual work and finite elements; introduction to elastic stability of columns; application of energy methods to determine stresses, strains and displacements in typical aerospace structures; design considerations in aerospace structures. Prerequisite: AERO 304.
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3.00 Credits
theory of free and forced vibrations and dynamic response of single and multi-degree of freedom systems; frequency response of first and second order systems with instrumentation applications. Prerequisites: AERO 30 or registratin therein; AERO 14, MATH 308.
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3.00 Credits
and analytical methods of solving engineering problems involving curve fitting; interpolation and extrapolation; difference operators and differentiation; integration; solutions to linear and non-linear equations and differential equations with engineering applications. Prerequisite: AERO 0; MATH 308 or registration therein.
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3.00 Credits
of gases; laws of thermodynamics; equilibrium conditions; mixtures of gases; combustion and thermochemistry; compressible internal flows with friction, heat transfer and shock; turbojet cycle analysis and performance; chemical rockets. Prerequisite: AERO 303 or registration therein.
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3.00 Credits
Aerospace Vehicle Design I. (2-3). Credit 3. Aerodynamic design, specification, arrangement, performance analysis, weight and balance, stability. Prerequisites: AERO 302, 303, 306, 351, 421.
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2.00 Credits
Aerospace Vehicle Design II. (0-6). Credit 2. Continuation of AERO 401. System optimization by examination and analysis of necessary trade-offs. Prerequisites: AERO 305, 401.
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