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Gas Turbines Internal Flow Systems Modeling

Gas Turbines Internal Flow Systems Modeling

Gas Turbines Internal Flow Systems Modeling is the culmination of three decades of continuous learning in gas turbine industry and a decade of teaching graduate-level courses in turbo machinery and fluid mechanics at UCF. It has taken this long for me to study the fascinating, and sometimes counter-intuitive, world of gas turbine secondary flow systems to the point that I can present the most complex topics in a simplified way that will make learning these topics contagious.

This is the age of gas turbines with their ever-growing contributions to people’s living standard and well-being. As a great technological marvel, perhaps next only to the inventions of electricity and light bulb, gas turbines have become indispensable in commercial aviation, shrinking the travel time around the globe in hours rather than days and weeks as was the case in the early 1990 s by sea. Almost all modern military fighter jets with high maneuverability deploy gas turbine engines. Even in liquid rocket propulsion, gas turbines are used to pump liquid fuel and oxidizer to the combustion chamber at high pressure.

You can also Read Pumps and compressors 2019

Gas Turbines Internal Flow Systems Modeling

  • Preface pageGas Turbines Internal Flow Systems Modeling
  • Acknowledgments
  • About the Author
  • Overview of Gas Turbines for Propulsion and Power Generation
  • Review of Thermodynamics, Fluid Mechanics, and Heat Transfer
  • Flow and Network Modeling
  • Internal Flow around Rotors and Sta-tors
  • Labyrinth Seals
  • Whole Engine Modeling
  • A:Review of Necessary Mathematics
  • B:Equations of Air Thermo-physical Properties
  • C:Transient Heat Transfer in a Rotor Disk
  • D:Regular Falsie Method
  • E:Thomas Algorithm for Solving a Tridiagonal System of Linear Algebraic Equations
  • F:Solution of an Over determined System of Linear Algebraic Equations
  • Epilogue Current Research Work and Challenges
  • Index

The book employs physics-based, design-oriented methodology to compute windage and swirl distributions in a complex rotor cavity formed by surfaces with arbitrary rotation, counter-rotation, and no rotation.


Gas Turbines Internal Flow Systems Modeling

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