- Jul 28, 2023
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Thomas Lambert authored
This completes the work started in !4 by implementing the true Reynolds recalculation for the other three solvers. Note that special care had to be implemented in Stahlhut solver in order to ensure proper numerical resolution of the solution.
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- Jul 27, 2023
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Rakotondratsimba Lyraie authored
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Rakotondratsimba Lyraie authored
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Rakotondratsimba Lyraie authored
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Rakotondratsimba Lyraie authored
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Rakotondratsimba Lyraie authored
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Rakotondratsimba Lyraie authored
calculate reynolds number exact value in indvel.m use its exact value when possible, if not use an approximation in ElemPerf.m
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- Jul 26, 2023
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Rakotondratsimba Lyraie authored
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- Jun 07, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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- May 31, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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- May 30, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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- May 26, 2023
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Thomas Lambert authored
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- May 25, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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- May 23, 2023
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Thomas Lambert authored
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- May 19, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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- May 18, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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- May 17, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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Thomas Lambert authored
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- May 16, 2023
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Thomas Lambert authored
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Thomas Lambert authored
The root cutout is at 5ft, then the blade morphs towards a cylinder of 3ft radius. So the blade actually stops at 5ft and not 3. As described in page 19, the non-dimensionalization uses a factor 1/2. This factor is associated with the "European" convention, while it does not appear in the US one (see Leishman, Principles of Helicopter Aeroydnamics, Eq 2.36).
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- Apr 28, 2023
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Thomas Lambert authored
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- Apr 26, 2023
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Thomas Lambert authored
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Thomas Lambert authored
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