Author: E. BaskharonePublisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Flow in Nonrotating Passages of Radial Inflow Turbines
Author: E. BaskharonePrinciples of Turbomachinery in Air-Breathing Engines
Author: Erian A. BaskharonePublisher: Cambridge University Press
ISBN: 0521858100
Category : Science
Languages : en
Pages : 599
Book Description
This book is intended for advanced undergraduate and graduate students in mechanical and aerospace engineering taking a course commonly called Principles of Turbomachinery or Aerospace Propulsion. The book begins with a review of basic thermodynamics and fluid mechanics principles to motive their application to aerothermodynamics and real-life design issues. This approach is ideal for the reader who will face practical situations and design decisions in the gas turbine industry. The text is fully supported by over 200 figures, numerous examples, and homework problems.
Flow in Primary, Non-rotating Passages in Turbomachines
Author: H. J. HerringPublisher:
ISBN:
Category : Science
Languages : en
Pages : 202
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
ASME Technical Papers
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 596
Book Description
Thermal Science
Author: Erian A. BaskharonePublisher: McGraw Hill Professional
ISBN: 0071772340
Category : Science
Languages : en
Pages : 482
Book Description
A practical, illustrated guide to thermal science A practical, illustrated guide to thermal science Written by a subject-matter expert with many years of academic and industrial experience, Thermal Science provides detailed yet concise coverage of thermodynamics, fluid mechanics, and heat transfer. The laws of thermodynamics are discussed with emphasis on their real-world applications. This comprehensive resource clearly presents the flow-governing equations of fluid mechanics, including those of mass, linear momentum, and energy conservation. Flow behavior through turbomachinery components is also addressed. The three modes of heat transfer--conduction, convection, and radiation--are described along with practical applications of each. Thermal Science covers: Properties of pure substances and ideal gases First and second laws of thermodynamics Energy conversion by cycles Power-absorbing cycles Gas power cycles Flow-governing equations External and internal flow structures Rotating machinery fluid mechanics Variable-geometry turbomachinery stages Prandtl-Meyer flow Internal flow, friction, and pressure drop Fanno flow process for a viscous flow field Rayleigh flow Heat conduction and convection Heat exchangers Transfer by radiation Instructor material available for download from companion website
Paper
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 598
Book Description
Applied Mechanics Reviews
Author: Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine
Author: Jianhui QiPublisher: Springer Nature
ISBN: 9811928606
Category : Technology & Engineering
Languages : en
Pages : 310
Book Description
To protect the Earth, China has launched its target of peaking carbon dioxide emissions by 2030, and achieving carbon neutrality by 2060 , which greatly encourages the use and development of renewable energy. Supercritical CO2 power cycle is a promising technology and the radial inflow turbine is the most important component of it, whose design and optimisation are considered as great challenges. This book introduces simulation tools and methods for supercritical CO2 radial inflow turbine, including a high fidelity quasi-one-dimensional design procedure, a non-ideal compressible fluid dynamics Riemann solver within open-source CFD software OpenFOAM framework, and a multi-objective Nelder–Mead geometry optimiser. Enhanced one-dimensional loss models are presented for providing a new insight towards the preliminary design of the supercritical CO2 radial inflow turbine. Since the flow phenomena within the blade channels are complex, involving fluid flow, shock wave transmission and boundary layer separation, only employing the ideal gas model is inadequate to predict the performance of the turbine. Thus, a non-ideal compressible fluid dynamics Riemann solver based on OpenFOAM library is developed. This book addresses the issues related to the turbine design and blade optimization and provides leading techniques. Hence, this book is of great value for the readers working on the supercritical CO2 radial inflow turbine and understanding the knowledge of CFD and turbomachinery.
Author: