Real Gas Simulations of a Sub-Scale Liquid Rocket Engine: Unsteady Simulations and Transient Heat Transfer in a Real Gas Environment

 
9783639199031: Real Gas Simulations of a Sub-Scale Liquid Rocket Engine: Unsteady Simulations and Transient Heat Transfer in a Real Gas Environment
Vedi tutte le copie di questo ISBN:
 
 

The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditions. Especially, the departure from ideal gas (because of cryogenic injection) is one of the major hurdle for such simulations. In order to begin addressing these issue, a real-gas model has been implemented in a massively parallel flow solver. This solver is capable of performing Large-Eddy Simulations in geometrical configurations ranging from an axisymmetric slice to a 3D slice up to a full 3D combustor. Results show the importance of the unsteady dynamics of the flow, especially the interaction between the different injectors. The role of the Peng-Robinson equation of state is assessed and the real gas model, despite a limited zone of application, seems to have a strong influence on the overall chamber behavior. This work also reviews in details the state of our knowledge on supercritical combustion in a coaxial injector configuration. We finally propose a comprehensive roadmap towards the completion of this goal and the possible use of CFD as a design tool for a modern liquid rocket engine.

Le informazioni nella sezione "Riassunto" possono far riferimento a edizioni diverse di questo titolo.

I migliori risultati di ricerca su AbeBooks

Foto dell'editore

1.

Matthieu Masquelet
Editore: VDM Verlag (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo PAP Quantità: 15
Print on Demand
Da
Paperbackshop-US
(Wood Dale, IL, U.S.A.)
Valutazione libreria

Descrizione libro VDM Verlag, 2010. PAP. Condizione: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Codice articolo LQ-9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 71,46
Convertire valuta

Aggiungere al carrello

Spese di spedizione: GRATIS
In U.S.A.
Destinazione, tempi e costi
Foto dell'editore

2.

Matthieu Masquelet
Editore: VDM Verlag Dr. Müller (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo Taschenbuch Quantità: 1
Da
Rheinberg-Buch
(Bergisch Gladbach, Germania)
Valutazione libreria

Descrizione libro VDM Verlag Dr. Müller, 2010. Taschenbuch. Condizione: Neu. Neuware - The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditions. Especially, the departure from ideal gas (because of cryogenic injection) is one of the major hurdle for such simulations. In order to begin addressing these issue, a real-gas model has been implemented in a massively parallel flow solver. This solver is capable of performing Large-Eddy Simulations in geometrical configurations ranging from an axisymmetric slice to a 3D slice up to a full 3D combustor. Results show the importance of the unsteady dynamics of the flow, especially the interaction between the different injectors. The role of the Peng-Robinson equation of state is assessed and the real gas model, despite a limited zone of application, seems to have a strong influence on the overall chamber behavior. This work also reviews in details the state of our knowledge on supercritical combustion in a coaxial injector configuration. We finally propose a comprehensive roadmap towards the completion of this goal and the possible use of CFD as a design tool for a modern liquid rocket engine. 168 pp. Englisch. Codice articolo 9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 68,00
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 17,13
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

3.

Matthieu Masquelet
Editore: VDM Verlag Dr. Müller (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo Taschenbuch Quantità: 1
Da
BuchWeltWeit Inh. Ludwig Meier e.K.
(Bergisch Gladbach, Germania)
Valutazione libreria

Descrizione libro VDM Verlag Dr. Müller, 2010. Taschenbuch. Condizione: Neu. Neuware - The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditions. Especially, the departure from ideal gas (because of cryogenic injection) is one of the major hurdle for such simulations. In order to begin addressing these issue, a real-gas model has been implemented in a massively parallel flow solver. This solver is capable of performing Large-Eddy Simulations in geometrical configurations ranging from an axisymmetric slice to a 3D slice up to a full 3D combustor. Results show the importance of the unsteady dynamics of the flow, especially the interaction between the different injectors. The role of the Peng-Robinson equation of state is assessed and the real gas model, despite a limited zone of application, seems to have a strong influence on the overall chamber behavior. This work also reviews in details the state of our knowledge on supercritical combustion in a coaxial injector configuration. We finally propose a comprehensive roadmap towards the completion of this goal and the possible use of CFD as a design tool for a modern liquid rocket engine. 168 pp. Englisch. Codice articolo 9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 68,00
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 17,13
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

4.

Masquelet, Matthieu
Editore: VDM Verlag 2010-02 (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo PF Quantità: 1
Da
Chiron Media
(Wallingford, Regno Unito)
Valutazione libreria

Descrizione libro VDM Verlag 2010-02, 2010. PF. Condizione: New. Codice articolo 6666-LSI-9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 70,45
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 17,35
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

5.

Masquelet, Matthieu
Editore: VDM Verlag (2017)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo Paperback Quantità: > 20
Print on Demand
Da
Ria Christie Collections
(Uxbridge, Regno Unito)
Valutazione libreria

Descrizione libro VDM Verlag, 2017. Paperback. Condizione: New. PRINT ON DEMAND Book; New; Publication Year 2017; Fast Shipping from the UK. No. book. Codice articolo ria9783639199031_lsuk

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 82,14
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 8,09
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

6.

Matthieu Masquelet
Editore: VDM Verlag (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo PAP Quantità: 15
Print on Demand
Da
Books2Anywhere
(Fairford, GLOS, Regno Unito)
Valutazione libreria

Descrizione libro VDM Verlag, 2010. PAP. Condizione: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Codice articolo LQ-9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 70,08
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 28,93
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi
Immagini fornite dal venditore

7.

Masquelet, Matthieu
Editore: VDM Verlag Dr. Müller (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo Kartoniert / Broschiert Quantità: > 20
Da
moluna
(Greven, Germania)
Valutazione libreria

Descrizione libro VDM Verlag Dr. Müller, 2010. Kartoniert / Broschiert. Condizione: New. The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditi. Codice articolo 151370284

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 55,52
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 45,00
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Immagini fornite dal venditore

8.

Matthieu Masquelet
Editore: VDM Verlag Dr. Müller (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo Taschenbuch Quantità: 1
Da
AHA-BUCH GmbH
(Einbeck, Germania)
Valutazione libreria

Descrizione libro VDM Verlag Dr. Müller, 2010. Taschenbuch. Condizione: Neu. Druck auf Anfrage Neuware - The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditions. Especially, the departure from ideal gas (because of cryogenic injection) is one of the major hurdle for such simulations. In order to begin addressing these issue, a real-gas model has been implemented in a massively parallel flow solver. This solver is capable of performing Large-Eddy Simulations in geometrical configurations ranging from an axisymmetric slice to a 3D slice up to a full 3D combustor. Results show the importance of the unsteady dynamics of the flow, especially the interaction between the different injectors. The role of the Peng-Robinson equation of state is assessed and the real gas model, despite a limited zone of application, seems to have a strong influence on the overall chamber behavior. This work also reviews in details the state of our knowledge on supercritical combustion in a coaxial injector configuration. We finally propose a comprehensive roadmap towards the completion of this goal and the possible use of CFD as a design tool for a modern liquid rocket engine. 168 pp. Englisch. Codice articolo 9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 68,00
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 34,50
Da: Germania a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

9.

Matthieu Masquelet
Editore: VDM Verlag, Germany (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo Paperback Quantità: 10
Da
The Book Depository EURO
(London, Regno Unito)
Valutazione libreria

Descrizione libro VDM Verlag, Germany, 2010. Paperback. Condizione: New. Language: English. Brand new Book. The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditions. Especially, the departure from ideal gas (because of cryogenic injection) is one of the major hurdle for such simulations. In order to begin addressing these issue, a real-gas model has been implemented in a massively parallel flow solver. This solver is capable of performing Large-Eddy Simulations in geometrical configurations ranging from an axisymmetric slice to a 3D slice up to a full 3D combustor. Results show the importance of the unsteady dynamics of the flow, especially the interaction between the different injectors. The role of the Peng-Robinson equation of state is assessed and the real gas model, despite a limited zone of application, seems to have a strong influence on the overall chamber behavior. This work also reviews in details the state of our knowledge on supercritical combustion in a coaxial injector configuration. We finally propose a comprehensive roadmap towards the completion of this goal and the possible use of CFD as a design tool for a modern liquid rocket engine. Codice articolo AAV9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 111,46
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 5,79
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi
Foto dell'editore

10.

Masquelet, Matthieu
Editore: - - (2010)
ISBN 10: 3639199030 ISBN 13: 9783639199031
Nuovo - Quantità: 20
Da
Chiron Media
(Wallingford, Regno Unito)
Valutazione libreria

Descrizione libro - -, 2010. Condizione: New. Codice articolo 6666-ING-9783639199031

Informazioni sul venditore | Contattare il venditore

Compra nuovo
EUR 106,04
Convertire valuta

Aggiungere al carrello

Spese di spedizione: EUR 17,35
Da: Regno Unito a: U.S.A.
Destinazione, tempi e costi