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Interaction between two oscillating stream in reactive system: Suppression of thermo-acoustic instabilities as studied using Fluid Image Velocimetry - Tapa blanda

 
9783846540800: Interaction between two oscillating stream in reactive system: Suppression of thermo-acoustic instabilities as studied using Fluid Image Velocimetry

Sinopsis

The performance requirements of any combustion system include maintaining a stable combustion over the entire operating range of fuel/air rates. Sometimes the operating range of the combustor is limited by large pressure oscillations and energy release fluctuations. Combustion instability is a common problem for almost all combustion devices in a wide range of applications: from rocket engine to industrial burners. It may take place in combustion chambers of various sizes and purposes using gaseous, liquid or solid fuel. The interaction between two oscillating streams as related to the suppression of the combustion instability was investigated. The ability of the tested configurations to suppress the low frequency combustion instability was demonstrated experimentally. Special emphasis was given to diagnostic techniques for analysis of the details of the oscillating streams and their interaction. An advanced method, with highly improved resolution and dynamic range FIV (Fluid Image Velocimetry) was specifically developed for this purpose and applied for velocity field analysis coupled with local measurements of time dependent pressure, temperature, CH*- emission and velocity.

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Reseña del editor

The performance requirements of any combustion system include maintaining a stable combustion over the entire operating range of fuel/air rates. Sometimes the operating range of the combustor is limited by large pressure oscillations and energy release fluctuations. Combustion instability is a common problem for almost all combustion devices in a wide range of applications: from rocket engine to industrial burners. It may take place in combustion chambers of various sizes and purposes using gaseous, liquid or solid fuel. The interaction between two oscillating streams as related to the suppression of the combustion instability was investigated. The ability of the tested configurations to suppress the low frequency combustion instability was demonstrated experimentally. Special emphasis was given to diagnostic techniques for analysis of the details of the oscillating streams and their interaction. An advanced method, with highly improved resolution and dynamic range FIV (Fluid Image Velocimetry) was specifically developed for this purpose and applied for velocity field analysis coupled with local measurements of time dependent pressure, temperature, CH*- emission and velocity.

Biografía del autor

Boris Golovanevsky received his Ph.D and Master degrees in Aerospace Engineering Department from Technion - Israel Institute of Technology in 1995 and 2004 respectively. He received Master degrees in Industrial Thermo-Technical School from National Polytechnical University of Odessa in 1990.

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  • EditorialLAP LAMBERT Academic Publishing
  • Año de publicación2011
  • ISBN 10 3846540803
  • ISBN 13 9783846540800
  • EncuadernaciónTapa blanda
  • IdiomaInglés
  • Número de páginas208
  • Contacto del fabricanteno disponible

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Boris Golovanevsky
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846540803 ISBN 13: 9783846540800
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Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Golovanevsky BorisBoris Golovanevsky received his Ph.D and Master degrees in Aerospace Engineering Department from Technion - Israel Institute of Technology in 1995 and 2004 respectively. He received Master degrees in Industrial Ther. Nº de ref. del artículo: 5497770

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Boris Golovanevsky
ISBN 10: 3846540803 ISBN 13: 9783846540800
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Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The performance requirements of any combustion system include maintaining a stable combustion over the entire operating range of fuel/air rates. Sometimes the operating range of the combustor is limited by large pressure oscillations and energy release fluctuations. Combustion instability is a common problem for almost all combustion devices in a wide range of applications: from rocket engine to industrial burners. It may take place in combustion chambers of various sizes and purposes using gaseous, liquid or solid fuel. The interaction between two oscillating streams as related to the suppression of the combustion instability was investigated. The ability of the tested configurations to suppress the low frequency combustion instability was demonstrated experimentally. Special emphasis was given to diagnostic techniques for analysis of the details of the oscillating streams and their interaction. An advanced method, with highly improved resolution and dynamic range FIV (Fluid Image Velocimetry) was specifically developed for this purpose and applied for velocity field analysis coupled with local measurements of time dependent pressure, temperature, CH - emission and velocity. 208 pp. Englisch. Nº de ref. del artículo: 9783846540800

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Boris Golovanevsky
Publicado por LAP LAMBERT Academic Publishing, 2011
ISBN 10: 3846540803 ISBN 13: 9783846540800
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Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The performance requirements of any combustion system include maintaining a stable combustion over the entire operating range of fuel/air rates. Sometimes the operating range of the combustor is limited by large pressure oscillations and energy release fluctuations. Combustion instability is a common problem for almost all combustion devices in a wide range of applications: from rocket engine to industrial burners. It may take place in combustion chambers of various sizes and purposes using gaseous, liquid or solid fuel. The interaction between two oscillating streams as related to the suppression of the combustion instability was investigated. The ability of the tested configurations to suppress the low frequency combustion instability was demonstrated experimentally. Special emphasis was given to diagnostic techniques for analysis of the details of the oscillating streams and their interaction. An advanced method, with highly improved resolution and dynamic range FIV (Fluid Image Velocimetry) was specifically developed for this purpose and applied for velocity field analysis coupled with local measurements of time dependent pressure, temperature, CH - emission and velocity. Nº de ref. del artículo: 9783846540800

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Boris Golovanevsky
ISBN 10: 3846540803 ISBN 13: 9783846540800
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Taschenbuch. Condición: Neu. Neuware -The performance requirements of any combustion system include maintaining a stable combustion over the entire operating range of fuel/air rates. Sometimes the operating range of the combustor is limited by large pressure oscillations and energy release fluctuations. Combustion instability is a common problem for almost all combustion devices in a wide range of applications: from rocket engine to industrial burners. It may take place in combustion chambers of various sizes and purposes using gaseous, liquid or solid fuel. The interaction between two oscillating streams as related to the suppression of the combustion instability was investigated. The ability of the tested configurations to suppress the low frequency combustion instability was demonstrated experimentally. Special emphasis was given to diagnostic techniques for analysis of the details of the oscillating streams and their interaction. An advanced method, with highly improved resolution and dynamic range FIV (Fluid Image Velocimetry) was specifically developed for this purpose and applied for velocity field analysis coupled with local measurements of time dependent pressure, temperature, CH\*- emission and velocity.Books on Demand GmbH, Überseering 33, 22297 Hamburg 208 pp. Englisch. Nº de ref. del artículo: 9783846540800

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Boris Golovanevsky
Publicado por Editorial Academica Espanola, 2011
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Condición: New. Print on Demand pp. 208 2:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on Creme w/Gloss Lam. Nº de ref. del artículo: 95317789

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Condición: New. PRINT ON DEMAND pp. 208. Nº de ref. del artículo: 1898160840

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