Stability Limits and Efficiency of Swirl-can Combustor Modules Burning Natural Gas Fuel

Stability Limits and Efficiency of Swirl-can Combustor Modules Burning Natural Gas Fuel PDF Author: Nicholas R. Marchionna
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28

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Stability Limits of a Methane-fueled Swirl Combustor

Stability Limits of a Methane-fueled Swirl Combustor PDF Author: Daniel Thomas Martin
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 166

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Laser Velocimetry Measurements in a Methane-fueled Swirl Combustor

Laser Velocimetry Measurements in a Methane-fueled Swirl Combustor PDF Author: James Stephen Depsky
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 244

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Combustion Noise

Combustion Noise PDF Author: Anna Schwarz
Publisher: Springer Science & Business Media
ISBN: 3642020380
Category : Technology & Engineering
Languages : en
Pages : 304

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Book Description
November, 2008 Anna Schwarz, Johannes Janicka In the last thirty years noise emission has developed into a topic of increasing importance to society and economy. In ?elds such as air, road and rail traf?c, the control of noise emissions and development of associated noise-reduction techno- gies is a central requirement for social acceptance and economical competitiveness. The noise emission of combustion systems is a major part of the task of noise - duction. The following aspects motivate research: • Modern combustion chambers in technical combustion systems with low pol- tion exhausts are 5 - 8 dB louder compared to their predecessors. In the ope- tional state the noise pressure levels achieved can even be 10-15 dB louder. • High capacity torches in the chemical industry are usually placed at ground level because of the reasons of noise emissions instead of being placed at a height suitable for safety and security. • For airplanes the combustion emissions become a more and more important topic. The combustion instability and noise issues are one major obstacle for the introduction of green technologies as lean fuel combustion and premixed burners in aero-engines. The direct and indirect contribution of combustion noise to the overall core noise is still under discussion. However, it is clear that the core noise besides the fan tone will become an important noise source in future aero-engine designs. To further reduce the jet noise, geared ultra high bypass ratio fans are driven by only a few highly loaded turbine stages.

Approaches for Clean Combustion in Gas Turbines

Approaches for Clean Combustion in Gas Turbines PDF Author: Medhat A. Nemitallah
Publisher: Springer Nature
ISBN: 303044077X
Category : Technology & Engineering
Languages : en
Pages : 426

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Book Description
This book focuses on the development of novel combustion approaches and burner designs for clean power generation in gas turbines. It shows the reader how to control the release of pollutants to the environment in an effort to reduce global warming. After an introduction to global warming issues and clean power production for gas turbine applications, subsequent chapters address premixed combustion, burner designs for clean power generation, gas turbine performance, and insights on gas turbine operability. Given its scope, the book can be used as a textbook for graduate-level courses on clean combustion, or as a reference book to accompany compact courses for mechanical engineers and young researchers around the world.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 402

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 582

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Thermoacoustic Combustion Instability Control

Thermoacoustic Combustion Instability Control PDF Author: Dan Zhao
Publisher: Academic Press
ISBN: 0323899188
Category : Technology & Engineering
Languages : en
Pages : 1145

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Book Description
Thermoacoustic Combustion Instability Control: Engineering Applications and Computer Codes provides a unique opportunity for researchers, students and engineers to access recent developments from technical, theoretical and engineering perspectives. The book is a compendium of the most recent advances in theoretical and computational modeling and the thermoacoustic instability phenomena associated with multi-dimensional computing methods and recent developments in signal-processing techniques. These include, but are not restricted to a real-time observer, proper orthogonal decomposition (POD), dynamic mode decomposition, Galerkin expansion, empirical mode decomposition, the Lattice Boltzmann method, and associated numerical and analytical approaches. The fundamental physics of thermoacoustic instability occurs in both macro- and micro-scale combustors. Practical methods for alleviating common problems are presented in the book with an analytical approach to arm readers with the tools they need to apply in their own industrial or research setting. Readers will benefit from practicing the worked examples and the training provided on computer coding for combustion technology to achieve useful results and simulations that advance their knowledge and research. - Focuses on applications of theoretical and numerical modes with computer codes relevant to combustion technology - Includes the most recent modeling and analytical developments motivated by empirical experimental observations in a highly visual way - Provides self-contained chapters that include a comprehensive, introductory section that ensures any readers new to this topic are equipped with required technical terms

Jet Engine Exhaust Emissions of High-altitude Commercial Aircraft Projected to 1990

Jet Engine Exhaust Emissions of High-altitude Commercial Aircraft Projected to 1990 PDF Author: Jack Grobman
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 90

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Flame Structure and Stabilization in Premixed Swirl-stabilized Combustion

Flame Structure and Stabilization in Premixed Swirl-stabilized Combustion PDF Author: Craig L. Beyler
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 172

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