Searched for: subject%3A%22Rocket%255C+Engine%255C+Turbine%255C+Blades%22
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Sanghera, Bhupinder Singh (author)
Prior to the detailed design of turbines, turbomachinery engineers must rely on mean-line and throughflow models to come to a preliminary design. These models are based on empirical loss correlations and are often derived from cascade experiments and numerical analyses that are confined to the subsonic and transonic regime. Axial turbines for...
master thesis 2020