2015
DOI: 10.1155/2015/485302
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Impact of the Surface Morphology on the Combustion of Simulated Solid Rocket Motor

Abstract: An advanced and intensive computational solution development is integrated with an asymptotic technique, to examine the impact of the combustion surface morphology on the generated rotational flow field in a solid rocket chamber with wide ranges of forcing frequencies. The simulated rectangular chamber is closed at one end and is open at the aft end. The upper and lower walls are permeable to allow steady and unsteady injected air to generate internal flow mimicking the flow field of the combustion gases in re… Show more

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