Aero- and thermodynamics of compressible fluids in air-breathing and rocket engines. Performance and cycle analysis of air-breathing engines, emphasizing turbojets, turbofans, turboprops, and ramjets; space propulsion including rocket dynamics, thrust chamber thermodynamics, and propulsion performance; performance of axial-flow and centrifugal compressors; turbines; and the matching of engine components. Prerequisite: MAE 3210 and MAE 2100.

Coverage of the design process including project management, specifications, budgeting and case histories, Conceptual, preliminary, and detailed design phases. Technical proposal and report preparation and technical presentations. Organization of design teams to work on specific semester long mechanical design projects selected to illustrate the design process. Engineering 4th Year Standing or instructor permission.

Introduces continuum mechanics and mechanics of deformable solids. Vectors and cartesian tensors, stress, strain, deformation, equations of motion, constitutive laws, introduction to elasticity, thermal elasticity, viscoelasticity, plasticity, and fluids. Cross-listed as APMA 6020, AM 6020. Taught concurrently w/ CE 6720. Prerequisite: Instructor permission.

Historical introduction, standard atmosphere, basic aerodynamics, airfoils and wings, flight mechanics, stability and control, propulsion (airbreathing, rocket and space), orbital mechanics.

Normal stress and strain, thermal strain, shear stress, shear strain; stress and strain transformations; Mohr's circle for plane stress and strain; stresses due to combined loading; axially loaded members; torsion of circular and thin-walled closed sections; statically indeterminate systems; deformation, strains and stresses in beams; beam deflections; column stability. Prerequisites: MAE 2300 or CE 2300

Application of experimental methods for thermal-fluid behavior. Topics include fluid properties, pressure and buoyancy, jet momentum, dimensional analysis, pipe flow, data analysis, particle image velocimetry, and measurement uncertainty. The laboratory experience will include activities to reinforce principles from Thermodynamics (MAE 2100) and Fluid Mechanics (MAE 3210).  Corequisite: MAE 3210 OR MAE 3215 

Introduction to fluid flow concepts and equations; characteristics of a fluid; mass and momentum conservation equations; fluid statics including buoyancy; Reynolds¿ Transport Theorem; Bernoulli's equation; viscous effects; Couette and Poiseuille flow; pipe and internal flow systems; fluid power systems; external boundary layers; flow over objects and associated lift and drag forces.  Corequisite: APMA 3140 or equivalent. 

This course has been developed for general graduate students and advanced undergraduate students in engineering. Assuming only basic knowledge of matrix operations, differential equations and electric circuits, the course aims to introduce, through numerous examples, fundamental concepts and tools for the analysis and design of control systems.

Applies basic engineering science, design methods, and systems analysis to developing areas and current problems in mechanical engineering. Topics vary based on student and faculty interest. Prerequisite: 3rd or 4th year standing.

Applies basic engineering science, design methods, and systems analysis to developing areas and current problems in aerospace engineering. Topics vary based on student and faculty interest. Prerequisite: Third or Fourth-year standing.