A generalised model of burning of a solid rocket propellant based on kinetics of propellant has been developed. A complete set of variables has been formed after examining the existing models. Buckingham theorem provides the functional form of the model, such that the existing models are the subcases of this generalised model. This proposed model has been validated by an experimental data.
Abstract-Fuel is one of the research areas of major focus in recent days. This review paper is based on the principle that it may be possible to grow our way out of an energy crisis with renewable, recyclable plant-based fuels. In turbine aircraft, combustion process acts on fan blades that either turns a propeller or create thrust by accelerating gas.
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