Basic Information
Introduction to Turbomachinery, Review of Compressible Flow, Flow With Work Exchange, Euler Turbomachinery Equation, Velocity Diagrams, Energy Transfer, Dimensional Analysis, Concepts of Flow Guidance, Understanding Efficiency and Loss Mechanisms In Turbomachinery, Centrifugal Comfressors, Axial Flow Compressors, Heat Transfer in Gas Turbines, Thermal Management Techniques, Design of Hot Gas Path Components. Learning Outcomes# At The End of The Course The Student Will Understand 1. Hot Gas Path Components. 2. The Physics Associated With Turbomachinery Components Typically Encountered in Small Jet Engines. 3. How to Blend The Scientific Knowledge Acquired in The Primary Courses (e.g. Aerodynamics, Heat Transfer and Structures) in a Single Application. 4. How to Form a Strong Basis Towards Multi-disciplinary Turbomachinery Design and Analysis. 5. The Fluid Dynamicsof Turbo Machines to Analyze and Evaluate Design Decisions. Design Decisions.6. How to Apply The Knowledge Acquired in Fundamentals of Compressor Design Towards Small Jet Engines. 7. How to Apply The Knowledge Acquired In Fundamentals of Turbine Design Towards Small Jet Engines. 8. How to Evaluate The Turbine Gas-path Heat Transfer to Select An Appropriate Cooling System. 9. How to Analyze Various Multi-disciplinary Design Decisions.
Faculty: Aerospace Engineering
|Graduate Studies
Pre-required courses
(84314 - Viscous Flow and Heat Transfer and 84401 - Jet Engines 1) or (84314 - Viscous Flow and Heat Transfer and 85407 - Introduction to Jet Engines)