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IUTAM Symposium on Combustion in Supersonic Flows - Proceedings of the IUTAM Symposium held in Poitiers, France, 2-6 October 1995 (Paperback, Softcover reprint of the original 1st ed. 1997)
Loot Price: R5,750
Discovery Miles 57 500
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IUTAM Symposium on Combustion in Supersonic Flows - Proceedings of the IUTAM Symposium held in Poitiers, France, 2-6 October 1995 (Paperback, Softcover reprint of the original 1st ed. 1997)
Series: Fluid Mechanics and Its Applications, 39
Expected to ship within 10 - 15 working days
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This volume contains selected presentations of the IUTAM Symposium
on Combustion in Supersonic Flows' held in Poitiers at the Ecole
Nationale Superieure de Mecanique et d'Aerotechnique (ENSMA) from 2
to 6 October 1995. The presentations focus on four main topics
related to combustion in supersonic streams and practical issues
relevant to the development of new propulsion systems: fundamental
studies of premixed and unpremixed combustion, fluid dynamics
aspects of supersonic combustion, practical systems including
Scramjet, Ramaccelerators and Pulsed Detonation Engines, and the
application of detonation to propulsion. Important progress has
been made in the understanding of local mechanisms which allow
combustion to be stabilized in a supersonic flow; in particular,
various mechanisms controlled by mixing, chemical kinetics, viscous
heating and shock waves are now well identified. Despite the
difficulty of developing experimental work on supersonic
combustion, a good set of experimental data is now available,
allowing validation of theoretical analysis and models. The main
aspects of modelling of turbulent combustion in high speed flows
were discussed, including the influence of turbulent fluctuations
on the chemistry-controlled phase of combustion and the
applicability of flamelet models to high speed flows. The full
range of numerical approaches is covered including Direct Numerical
Simulation, Large Eddy Simulation, k-epsilon and shock tracking
methods. A considerable effort has been made to generalize these
methods to the treatment of supersonic reactive flows and to
develop new numerical methods taking into account the most recent
theoretical work and a better understanding of the underlying
physics."
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