Author: Janós M. BeérPublisher:
ISBN:
Category :
Languages : en
Pages : 274
Book Description
Combustion aerodynamics
Author: Janós M. BeérCombustion Aerodynamics
Author: János Miklós BeérPublisher:
ISBN:
Category : Science
Languages : en
Pages : 288
Book Description
Combustion Aerodynamics [by] J.M. Beér and N.A. Chigier
![Combustion Aerodynamics [by] J.M. Beér and N.A. Chigier PDF](https://books.google.com/books/content/images/frontcover/LQ3JtAEACAAJ?fife=w80-h100)
Author: János Miklós BeérPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 264
Book Description
Combustion Processes
Author: Bernard LewisPublisher: Princeton University Press
ISBN: 1400877024
Category : Science
Languages : en
Pages : 695
Book Description
Volume II of the High Speed Aerodynamics and Jet Propulsion series. This volume includes treatments of all aspects of combustion necessary to the development of jet and rocket engines. Originally published in 1956. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Aerodynamics for Naval Aviators
Author: U.S. Navy Naval Air Systems CommandPublisher: Ravenio Books
ISBN:
Category : Transportation
Languages : en
Pages : 510
Book Description
Combustion Aerodynamics
Author: George Appleton BallAerodynamics for Naval Aviators
Author: Hugh H. HurtPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 436
Book Description
Combustor Aerodynamics
Author: Yehia A. EldrainyPublisher: Penerbit UTM Press
ISBN: 9835208530
Category : Combustion, Theory of
Languages : en
Pages : 5
Book Description
This book describes the new innovation of gas turbine swirler. The novel swirler is a multiple entry swirler which allows the swirl number to vary on the same value of Reynolds number, by regulating the ratio between the axial and tangential flow momentum. Three–dimensional turbulence and isothermal flow characteristics of an abrupt combustor model with different type of swirler (axial, radial and multiple inlet) were simulated with Reynolds–Averaged Navier–Stokes (RANS) using ANSYS Fluent 12 software. Results of the different turbulence models used in swirling flow were reviewed and compared. The different swirler’ aerodynamic performance was investigated through Computational Fluid Dynamics (CFD) simulations. The aerodynamics performance includes shape and size of the Central Recirculation Zone (CRZ), turbulence intensity and pressure losses. It was found that the size of then CRZ and turbulence strength is directly proportional to the tangential axial air flow rate ratio. Therefore, proper selection of a swirler is needed to enhance combustor performance and to reduce exhaust emissions.
Mathematical Study of a Propagating Flame and Its Induced Aerodynamics in a Coal Mine Passageway
Author: Donald N. H. ChiPublisher:
ISBN:
Category : Coal mines and mining
Languages : en
Pages : 60
Book Description
Author: