Analysis team code used for the AIAA DBF 2025 competition.
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초기설정 가이드를 따라하기
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vsp_analysis.py에서 airfoil data path를 적절히 수정
s9027_path = r"C:\Path\to\DBF2025_SizingCode\VSP_analysis\s9027.dat"
naca0008_path = r"C:\Path\to\DBF2025_SizingCode\VSP_analysis\naca0008.dat"
- Anaylsis parameter 설정
vsp_file = os.path.join(vsp3_dir, "Mothership.vsp3")
alpha_start = -2.0 # Starting angle of attack (degrees)
alpha_end = 2.0 # Ending angle of attack (degrees)
alpha_step = 1.0 # Step size (degrees)
Re = 380000 # Reynolds number
Mach = 0 # Mach number (subsonic)