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AERO 212: Thermodynamics Aero Engr
3.00 Credits
Texas A & M University-Galveston
Thermodynamics for Aerospace Engineers. (2-2). Credit 3. Study of thermodynamic properties and processes, heat and work, first and second laws of thermodynamics, power and refrigeration ideal cycles, psychrometrics. Prerequisites: Admission to upper division degree sequence in aerospace engineering; AERO 209 or registration therein; MATH 308 or registration therein.
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AERO 212 - Thermodynamics Aero Engr
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AERO 213: Material Sci Aero Engr
3.00 Credits
Texas A & M University-Galveston
Material Science for Aerospace Engineers. (2-2). Credit 3. Study of the interrelations in engineering materials and their microstructure; study of structural, electrical, optical, thermal properties; study of structure-property relationships in terms of the engineering of materials. Prerequisites: Admission to upper division degree sequence in aerospace engineering; AERO 209 and MATH 251 or 253 or registration therein.
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AERO 213 - Material Sci Aero Engr
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AERO 214: Aero Continuum Mechanics
3.00 Credits
Texas A & M University-Galveston
Aerospace Engineering Principles of Continuum Mechanics. (2-2). Credit 3. Fundamental concepts and illustrative examples of conservation laws forming the framework upon which our description of engineering mechanics of deformable bodies is based; complex examination of the manner in which these principles are applied to selected traditional areas of engineering and their associated applications. Prerequisites: AERO 209; AERO 213 and MATH 308 or registration therein.
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AERO 214 - Aero Continuum Mechanics
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AERO 220: Intro Aero Computation
2.00 Credits
Texas A & M University-Galveston
Introduction to Aerospace Computation. (2-1). Credit 2. Introduction to the basic skills required for developing computer programs that solve aerospace engineering problems; engineering and math background from previous and concurrent courses will serve as the theoretical basis and motivation for programming assignments; an integrated development environment will be used for code writing, compilation, debugging, and organization. Prerequisites: Admission to upper division degree sequence in aerospace engineering; AERO 209 or registration therein.
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AERO 220 - Intro Aero Computation
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AERO 289: Special Topics In
1.00 - 4.00 Credits
Texas A & M University-Galveston
Special Topics in... Credit 1 to 4. Selected topics in an identified area of aerospace engineering. May be repeated for credit. Prerequisite: Approval of instructor.
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AERO 289 - Special Topics In
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AERO 291: Research
1.00 - 4.00 Credits
Texas A & M University-Galveston
Research. Credit 1 to 4. Research conducted under the direction of faculty member in aerospace engineering. May be repeated 3 times for credit. Prerequisites: Freshman or sophomore classification and approval of instructor.
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AERO 291 - Research
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AERO 301: Theoretical Aerodyn
3.00 Credits
Texas A & M University-Galveston
Theoretical Aerodynamics. (3-0). Credit 3. Fundamentals of incompressible flow, conservation principles, continuity, momentum, rotationality, circulation, lift, drag, potential flow, thin airfoil theory, panel methods, airfoil design, high lift devices, finite wing theory, vortex lattice methods, and wing design. Prerequisites: AERO 201, MATH 308; AERO 320 or registration therein.
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AERO 301 - Theoretical Aerodyn
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AERO 302: Aero Engr Lab I
2.00 Credits
Texas A & M University-Galveston
Aerospace Engineering Laboratory I. (1-3). Credit 2. Demonstrates 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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AERO 302 - Aero Engr Lab I
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AERO 303: High Speed Aerodyn
3.00 Credits
Texas A & M University-Galveston
High Speed Aerodynamics. (3-0). Credit 3. Fundamentals 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 212, 301.
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AERO 303 - High Speed Aerodyn
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AERO 304: Aero Structural Analys I
3.00 Credits
Texas A & M University-Galveston
Aerospace Structural Analysis I. (3-0). Credit 3. Structural design considerations; mechanics of structures; introduction to elasticity; constitution of materials; analysis of typical aerospace structures in bending, extension, torsion and shear. Prerequisites: AERO 320 or registration therein; AERO 213, 214, MATH 308.
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AERO 304 - Aero Structural Analys I
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