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This paper presents an analytical viscous flow model for swirl injectors used in rocket engines, addressing the limitations of traditional inviscid flow models that neglect viscosity effects. The new model incorporates viscous diffusion, leading to a more accurate prediction of injector performance, particularly for high-viscosity propellants like Ethanol. Experimental validation with Liquid Oxygen (LOX) and Ethanol demonstrates good agreement between the model and test results, facilitating the creation of
- Author
- clksila6106
- Language
- EN