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Turbomachine Unsteady Aerodynamics

Turbomachine Unsteady Aerodynamics

          
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About the Book

The problem of blade fatigue failures is important in the design of new gas turbines. The most important information required in estimating the blade life is the non-steady force field arising out of the stage flow path interaction. This book is concerned with such information.

Basic principles of inviscid incompressible flows are first presented with applications to elementary incompressible flows. The airfoil theory using conformal mapping is then given to explain the basic principles of steady aerodynamic lift followed by two dimensional thin airfoil theory. The unsteady thin airfoil theory due to transverse and chordwise gusts in the upstream flow is given in detail, which is then linked to the turbomachine stage flow. The blade lift and moment calculations arising out of potential flow and vortex wakes from the neighbouring row are then presented. Next, the principles of compressible flow are introduced with extension to the turbomachine stage problem. A modified exact hydraulic analogy for isentropic flows is then introduced to study flow path interaction in a gas turbine stage. Finally, viscous flow and boundary layer theory are introduced with applications to the turbomachine blades. Thus, this book enables a designer to determine the blade nonsteady force field in a turbomachine.

About The Author
Prof. J.S. Rao (Hons.), M. Tech, Ph.D., D.Sc, taught at the Indian Institute of Technology, Kharagpur and Delhi for over 30 years. He has also taught at the University of Surrey, as a Commonwealth Fellow; at National Institute of Applied Sciences, Lyon; Concordia University, Montreal; Rochester Institute of Technology and Gesamthoch schule in Kassel as Visiting Professor. Prof. Rao started a new Centre on Industrial Tribology, Machine Dynamics and Maintenance Engineering at IIT, Delhi in 1977. He also served as Science Counselor at the Indian Embassy in Washington during 1984-88.

Prof, Rao has been the Chairman of IFToMM Rotor Dynamics Committee from 1983-90 and is a member of IFToMM Executive Council and Chairman of IFToMM Commission on Conferences. Prof. Rao has been the Founder President of Association of Machines and Mechanisms in India and is the President of Indian Society of Theoretical and Applied Mechanics. He is a member of Indian National Academy of Engineering and American Society of Mechanical Engineers. He is also Chairman of Vibration and Rotor Dynamics Group of the Aeronautical Research and Development Board Propulsion Panel, and member of ASME IGT Structures and Dynamics Committee.

Prof. Rao produced 26 Ph.Ds and published 5 text books and over 200 papers. He has been a consultant to various organizations in India such as BHEL, GTRE and abroad such as Washington Metro Authority, Stress Technology Inc. etc. His biographical sketch is reviewed by Marquis Whos who, Men of Achievement, Whos who in Common wealth, Leaders in Education & Educationists Whos who International, and Reference Asia.

Table Of Contents

  • Introduction
  • Basic Principles of Inviscid Incompressible Flows
  • Elementary Incompressible Flows
  • Airfoil Theory by Mapping arid Using Flow Field over a Circular Cylinder
  • Two-Dimensional Thin Airfoil Theory
  • Airfoil in Unsteady Flow
  • Unsteady Aerodynamics of a Thin 2-0 Blade Stage in Incompressible Flow
  • Inviscid Compressible Flow
  • Subsonic Compressible Flow in 2-0 Thin Airfoil Stage
  • Hydraulic Analogy
  • Introduction to Viscous Flow and Boundary Layers
  • Unsteady Lift and Moment Due to Viscons Weaks.


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Product Details
  • ISBN-13: 9788122406535
  • Publisher: New Age
  • Binding: Hardcover
  • Language: English
  • ISBN-10: 812240653X
  • Publisher Date: 1994
  • Edition: 1st

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