LOW-REYNOLDS-NUMBER COMPRESSOR DEVIATION ANGLE MODEL BASED ON PHYSICS-ENHANCED TWO-STAGE SYMBOLIC REGRESSION APPROACH
Traditional compressor deviation angle models, primarily developed for NACA and double-circular-arc airfoils, cannot accurately predict the deviation characteristics of modern aerodynamically optimized blades and generally neglect Reynolds number (Re) and Mach number (Ma) effects, limiting their applicability to low-...