2D CFD Analysis of Combustion in Eight Legged Star Shaped Perforation - Couverture souple

Pandey, Krishna ; Deb, Sunita

9783659694905: 2D CFD Analysis of Combustion in Eight Legged Star Shaped Perforation

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ISBN 10 : 3659694908 ISBN 13 : 9783659694905

Editeur : LAP LAMBERT Academic Publishing, 2015

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Chemical rocket propellants undergo exothermic chemical reactions to produce hot gases which expand and push on a nozzle, which accelerates them until they rush out of the back of the rocket at extremely high speed. They can be basically classified into two types, liquid propellants and solid propellants. Solid propellants can be basically classified into double base propellant and composite propellant. Solid propellants are used in forms called grains. A grain is any individual particle of propellant regardless of the size or shape. The shape and size of a propellant grain determines the burn time, amount of gas and rate produced from the burning propellant and consequently thrust vs time profile. Most commonly used solid propellant is ammonium perchlorate composite propellant with Hydroxyl Terminated Polybutadiene (HTPB) binder. Ammonium perchlorate decomposes to give oxidizer molecules and HTPB decomposes to give out fuel molecules. The exothermic reactions that sustain the combustion process occur in solid, surface and the gaseous phase and thus comprise complex chemical kinetics.

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� propos de l'auteur

Professor Pandey received his B.Tech in Mechanical Engineering from IIT Varanasi n 1980, M.Tech in Heat Power in 1987 from the same institute in January 1987. He obtained Ph.D. in Mechanical Engineering from IIT,Kanpur in 1994.He has joined as faculty in Mechanical Engineering in the National Institute of Technology Silchar on 6th January 1987.

Les informations fournies dans la section � A propos du livre � peuvent faire r�f�rence � une autre �dition de ce titre.

�diteur: LAP LAMBERT Academic Publishing
Date d'�dition: 2015
Langue: anglais
ISBN 10: 3659694908
ISBN 13: 9783659694905
Reliure: Broch�
Nombre de pages: 92
Coordonn�es du fabricant: non disponible
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2D CFD Analysis of Combustion in Eight Legged Star Shaped Perforation

Krishna Pandey

Edit� par LAP LAMBERT Academic Publishing Apr 2015, 2015

ISBN 10 : 3659694908 ISBN 13 : 9783659694905

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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Chemical rocket propellants undergo exothermic chemical reactions to produce hot gases which expand and push on a nozzle, which accelerates them until they rush out of the back of the rocket at extremely high speed. They can be basically classified into two types, liquid propellants and solid propellants. Solid propellants can be basically classified into double base propellant and composite propellant. Solid propellants are used in forms called grains. A grain is any individual particle of propellant regardless of the size or shape. The shape and size of a propellant grain determines the burn time, amount of gas and rate produced from the burning propellant and consequently thrust vs time profile. Most commonly used solid propellant is ammonium perchlorate composite propellant with Hydroxyl Terminated Polybutadiene (HTPB) binder. Ammonium perchlorate decomposes to give oxidizer molecules and HTPB decomposes to give out fuel molecules. The exothermic reactions that sustain the combustion process occur in solid, surface and the gaseous phase and thus comprise complex chemical kinetics. 92 pp. Englisch. N� de r�f. du vendeur 9783659694905

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2D CFD Analysis of Combustion in Eight Legged Star Shaped Perforation

Krishna Pandey|Sunita Deb

Edit� par LAP LAMBERT Academic Publishing, 2015

ISBN 10 : 3659694908 ISBN 13 : 9783659694905

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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Pandey KrishnaProfessor Pandey received his B.Tech in Mechanical Engineering from IIT Varanasi n 1980, M.Tech in Heat Power in 1987 from the same institute in January 1987. He obtained Ph.D. in Mechanical Engineering from IIT,Kanpur . N� de r�f. du vendeur 26588780

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2D CFD Analysis of Combustion in Eight Legged Star Shaped Perforation

Krishna Pandey

Edit� par LAP LAMBERT Academic Publishing Apr 2015, 2015

ISBN 10 : 3659694908 ISBN 13 : 9783659694905

Neuf Taschenbuch

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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Chemical rocket propellants undergo exothermic chemical reactions to produce hot gases which expand and push on a nozzle, which accelerates them until they rush out of the back of the rocket at extremely high speed. They can be basically classified into two types, liquid propellants and solid propellants. Solid propellants can be basically classified into double base propellant and composite propellant. Solid propellants are used in forms called grains. A grain is any individual particle of propellant regardless of the size or shape. The shape and size of a propellant grain determines the burn time, amount of gas and rate produced from the burning propellant and consequently thrust vs time profile. Most commonly used solid propellant is ammonium perchlorate composite propellant with Hydroxyl Terminated Polybutadiene (HTPB) binder. Ammonium perchlorate decomposes to give oxidizer molecules and HTPB decomposes to give out fuel molecules. The exothermic reactions that sustain the combustion process occur in solid, surface and the gaseous phase and thus comprise complex chemical kinetics.VDM Verlag, Dudweiler Landstra�e 99, 66123 Saarbr�cken 92 pp. Englisch. N� de r�f. du vendeur 9783659694905

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2D CFD Analysis of Combustion in Eight Legged Star Shaped Perforation

Krishna Pandey

Edit� par LAP LAMBERT Academic Publishing, 2015

ISBN 10 : 3659694908 ISBN 13 : 9783659694905

Neuf Taschenbuch

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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Chemical rocket propellants undergo exothermic chemical reactions to produce hot gases which expand and push on a nozzle, which accelerates them until they rush out of the back of the rocket at extremely high speed. They can be basically classified into two types, liquid propellants and solid propellants. Solid propellants can be basically classified into double base propellant and composite propellant. Solid propellants are used in forms called grains. A grain is any individual particle of propellant regardless of the size or shape. The shape and size of a propellant grain determines the burn time, amount of gas and rate produced from the burning propellant and consequently thrust vs time profile. Most commonly used solid propellant is ammonium perchlorate composite propellant with Hydroxyl Terminated Polybutadiene (HTPB) binder. Ammonium perchlorate decomposes to give oxidizer molecules and HTPB decomposes to give out fuel molecules. The exothermic reactions that sustain the combustion process occur in solid, surface and the gaseous phase and thus comprise complex chemical kinetics. N� de r�f. du vendeur 9783659694905

Contacter le vendeur