Resources
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Extraordinary Results...
Coefficient of lift is calculated through explicit formula. Here you see; in real time as the tunnel runs multiple experiments, CL results less than 2.6% off the ideal. These results were later confirmed and incorporated into the final results. On experiment close, I was (literally) tackled by a professor saying these results are extraorinarily impressive and equally very uncommon.
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Off the Chart
What’s going on here; the (Dynamic Soaring) airframe just keeps going ever quicker. Designed for a pressure Q of 50, we raised it to 70.