Data and code for "Unified Momentum Model for Rotor Aerodynamics Across Operating Regimes"

This repository contains a reference implementation of the Unified Momentum Model presented in the associated manuscript titled **Unified Momentum Model for Rotor Aerodynamics Across Operating Regimes**. The Unified Momentum Model is a novel approach for modeling a yaw-misaligned actuator disk induction and outlet velocities, including negative and high thrust regimes.本代码仓库包含刊载于题为《跨运行工况旋翼空气动力学统一动量模型》的相关研究手稿中提出的统一动量模型（Unified Momentum Model）的参考实现。该统一动量模型是一种用于建模偏航失准致动盘（actuator disk）诱导速度与出口速度的创新方法，其涵盖负推力工况与高推力工况。