Hengky
Talino
Analysis
Initial Analysis
In the initial analysis conducted through XFLR5 software, the focus was on determining lift and drag coefficients to assess aerodynamic performance. Additionally, general aircraft stability parameters were examined, providing valuable insights into flight characteristics and potential design improvements.
Flow Analysis
In-depth analysis using ANSYS CFX software was employed to examine the flying characteristics of both individual wings and the entire airplane, as well as the empennage. The study resulted in the evaluation of total lift and drag, as well as stability factors that influenced wing features like sweep-back and dihedral
Structural Analysis
ANSYS Mechanical software was utilized for structural analysis, evaluating overall properties like equivalent stress and safety factor in the aircraft. This aimed to identify and address potential issues, informing design updates for enhanced structural integrity and safety.