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Template for the convergence study course in Coursera - Copy

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E13 aerodynamic analysis - Copy - Copy - Copy - Copy - Copy - Copy - Copy - Copy - Copy

To perform flutter analysis for a rocket fin. Solid mechanics and/or Fluid dynamics module will be used. The project is to make a rocket with a target of 3 km apogee with dual deployment recovery system.

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Making a set of better foils for my Waszp

assess pressure loss at different flow rates

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wing simulation - Copy - Copy - Copy - Copy - Copy - Copy - Copy

wing simulation - Copy - Copy - Copy - Copy - Copy - Copy - Copy - Copy

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