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Submitted
Boeing 737-300 - VLM - panel method
Calculation of Cl(y) and Cp(y) using VLM method.
mer än 4 år ago | 2 downloads |
Submitted
NACA 2412 - vortex divsion over the chord
NACA 2412 pressure on the upper and lower surface.
mer än 4 år ago | 3 downloads |
Submitted
NACA 00XX - doublet divison over the chord
NACA 00XX - doublet divison over the chord compard to Abbott & Von Doenhoff book.
mer än 4 år ago | 1 download |
Submitted
aeroelastic deformations efficiency - divergence speed
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow condition...
mer än 4 år ago | 5 downloads |