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Tamir Gazit


Last seen: bijna 2 jaar ago Active since 2020

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

meer dan 4 jaar ago | 2 downloads |

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Submitted


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

meer dan 4 jaar ago | 3 downloads |

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Submitted


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

meer dan 4 jaar ago | 1 download |

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Submitted


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

meer dan 4 jaar ago | 5 downloads |

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