Deflection Characteristics of Particles Traversing Oblique Shock Waves
摘要
To investigate the effects of rain/snow/hail particles on aircraft surfaces, this study analyzes particle trajectory deflection through hypersonic wedge shock layers and associated erosion distribution characteristics. We established governing equations via classical shock theory and introduced a Mach-adaptive drag coefficient model validated by CFD.The framework reveals parabolic post-shock deflection, exponentially decaying surface distributions, and monotonically decreasing impact angles/velocities along the flow direction, thereby providing a theoretical tool for leading-edge erosion-resistant design and lifespan prediction.