Mukunda, HS (1978) A Comprehensive Theory of Erosive Burning in Solid Rocket Propeilants. In: Combustion Science and Technology, 18 (3-4). 105-118 .Full text not available from this repository.
The theory of erosive burning has been constructed front first principles using turbulent boundary layer concepts. It is shown that the problem constitutes one of solution of flame propagation equation for turbulent flow. The final approximate solution for the case of single step overall kinetics reveals the combined effects of fluid mechanics and chemical kinetics. The results obtained from this theory are compared with earlier experimental results. The dependence of erosive burning characteristics on various parameters has been elucidated.
|Item Type:||Journal Article|
|Additional Information:||Copyright of this article belongs to Taylor and Francis Group.|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||06 Oct 2010 07:35|
|Last Modified:||06 Oct 2010 07:35|
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