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Xin'gen Lu

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Aug 2026

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-...

Ruo-Yu Chen, Cheng-Wu Yang, Li-Pan Yao et al. · 0 citations

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