Combustion aerodynamics PDF Download
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Author: Janós M. Beér
Publisher:
ISBN:
Category :
Languages : en
Pages : 274
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Book Description
Author: Janós M. Beér
Publisher:
ISBN:
Category :
Languages : en
Pages : 274
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Book Description
Author: János Miklós Beér
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 288
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Book Description
![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 Beér
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 264
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Book Description
Author: U.S. Navy Naval Air Systems Command
Publisher: Ravenio Books
ISBN:
Category : Transportation
Languages : en
Pages : 510
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Book Description
Author: Bernard Lewis
Publisher: Princeton University Press
ISBN: 1400877024
Category : Science
Languages : en
Pages : 695
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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.
Author: Hugh H. Hurt
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 436
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Book Description
Author: George Appleton Ball
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
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Book Description
Author: Donald N. H. Chi
Publisher:
ISBN:
Category : Coal mines and mining
Languages : en
Pages : 60
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Book Description
Author: Yehia A. Eldrainy
Publisher: Penerbit UTM Press
ISBN: 9835208530
Category : Combustion, Theory of
Languages : en
Pages : 5
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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.
Author: Ethirajan Rathakrishnan
Publisher: John Wiley & Sons
ISBN: 1118479378
Category : Technology & Engineering
Languages : en
Pages : 560
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Book Description
Theoretical Aerodynamics is a user-friendly text for a full course on theoretical aerodynamics. The author systematically introduces aerofoil theory, its design features and performance aspects, beginning with the basics required, and then gradually proceeding to higher level. The mathematics involved is presented so that it can be followed comfortably, even by those who are not strong in mathematics. The examples are designed to fix the theory studied in an effective manner. Throughout the book, the physics behind the processes are clearly explained. Each chapter begins with an introduction and ends with a summary and exercises. This book is intended for graduate and advanced undergraduate students of Aerospace Engineering, as well as researchers and Designers working in the area of aerofoil and blade design. Provides a complete overview of the technical terms, vortex theory, lifting line theory, and numerical methods Presented in an easy-to-read style making full use of figures and illustrations to enhance understanding, and moves well simpler to more advanced topics Includes a complete section on fluid mechanics and thermodynamics, essential background topics to the theory of aerodynamics Blends the mathematical and physical concepts of design and performance aspects of lifting surfaces, and introduces the reader to the thin aerofoil theory, panel method, and finite aerofoil theory Includes a Solutions Manual for end-of-chapter exercises, and Lecture slides on the book's Companion Website
