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Determination of The Deflector Wall Thickness and Influence of The Maximum Angle of Shock Wave On Heat Exchange in The Combustion Gases of Solid Particles by IJAET Journal is a document available to read on EtoBox.

When a rocket engine is burned, it is necessary to release the combustion products away from the burning area so as not to damage the equipment and structures located on the side. This work presents a flame deflector and combustion gas design in launching platform. Such a device is intended to divert the exhaust jets and absorb a fraction of the high rate of existing heat, due to the high temperature of gases from the burning of fuel in the rocket engine. In this type of problem, the determinati

Author

IJAET Journal

Language

EN