Tamir Gazit

Last seen: 2 years 前 | 自 2020 起处于活动状态

Followers: 0 Following: 0

All

已提交

Boeing 737-300 - VLM - panel method
Calculation of Cl(y) and Cp(y) using VLM method.

4 years 前 | 2 次下载 |

已提交

NACA 2412 - vortex divsion over the chord
NACA 2412 pressure on the upper and lower surface.

4 years 前 | 3 次下载 |

已提交

NACA 00XX - doublet divison over the chord
NACA 00XX - doublet divison over the chord compard to Abbott & Von Doenhoff book.

4 years 前 | 1 次下载 |

已提交

aeroelastic deformations efficiency - divergence speed
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow condition...

4 years 前 | 5 次下载 |

Explorer