Steady VLM correction exemplar

This dataset includes an example MATLAB script that implements corrections to steady Vortex Lattice Method (VLM) results. Corrections include: Viscous lift curve slope. Lifting surface viscous drag (including lift-dependent viscous drag). Fuselage profile drag. Fuselage contribution to pitching moment. Tailplane contribution to pitching moment. The example includes experimental wind tunnel data from a model of an English Electric Canberra, along with software models of this aircraft in three popular steady VLM solvers: AVL, XFLR5 and OpenVSP/VSPAERO.本数据集包含一段用于对定常涡格法（Vortex Lattice Method, VLM）计算结果进行修正的示例MATLAB脚本。需修正的内容包括： 1. 黏性升力曲线斜率修正； 2. 升力面黏性阻力（含升致黏性阻力）修正； 3. 机身型阻修正； 4. 机身对俯仰力矩的贡献修正； 5. 平尾对俯仰力矩的贡献修正。 本示例附带了英国电气堪培拉（English Electric Canberra）机型模型的风洞实验数据，以及三款主流定常涡格法求解器——AVL、XFLR5与OpenVSP/VSPAERO——针对该机型的软件模型。