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A data-driven non-intrusive polynomial chaos for performance impact of high subsonic compressor cascades with stagger angle and profile errors

Numerical AnalysisAeroacousticsCompressible FlowEngineeringProfile ErrorsAerospace EngineeringCompressorPerformance ImpactNonlinear Signal ProcessingComputational MechanicsStagger AngleNonlinear AcousticSupersonic Combustion