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Low Speed Airfoil Design. Joan Puig. Project Goals. Maximize L/D Easy to build Keep Cm at a value that is not going to make the airplane unstable Have space for a strong structure Design an optimal airfoil for my RC airplane. Tools. Panel Method to generate Cp distribution
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Low Speed Airfoil Design Joan Puig
Project Goals • Maximize L/D • Easy to build • Keep Cm at a value that is not going to make the airplane unstable • Have space for a strong structure • Design an optimal airfoil for my RC airplane
Tools • Panel Method to generate Cp distribution • Shape adjusting function • Optimizer • Drag estimation tools (future work...)
Shape Adjusting Function • It generates any reasonable airfoil starting from a guess and a set of linerly independent bump functions.
Optimization Process Review • Don't assume anything about the input data • Fit the input data using a spline to the desired X coordinate values • Pass appropriate parameters to the optimization function • Collect data periodically
Speed • Solving a matrix is o(n^3) -> most of the time is spent here • Try to be able to fit your matrix in the cache • 32*(n^2+8n)/(8*1024)<available cache ~128-512 • Don't calculate x^2, x^3, sin(...) exp(...^n)... every time, compute them at the beginning and use them as global variables