Aerodynamic Data for Validation: The CHN-T1 Large Aircraft Standard Model Dataset

Each individual polar test run is saved as a standalone, comma-separated values (.csv) file in the corresponding subdirectory, with columns arranged in a consistent sequential order of freestream Mach number (Ma), model angle of attack (Alpha), model sideslip angle (Beta), unit Reynolds number (Re), lift coefficient (CL), drag coefficient (CD), pitching moment coefficient (Cm), normal force coefficient (CN), axial force coefficient (CA) , side force coefficient (CY), yawing moment coefficient (Cn) and rolling moment coefficient (Cl); this universal, consistent data format across the entire dataset enables simplified batch reading, automated processing, and seamless post-processing for aerodynamic analysis.