No, I actually ran a compete series of tests of a symmetrical NASA wing shape in a small wind tunnel through different angles of attack, and wind speeds/Reynolds numbers. The wing was instrumented with 10 air pressure tubes on the top and bottom. I developed a computer program to compute the aerodynamic lift and drag from the pressure data on each run. At the same time, a strain gauge measured actual total lift on the mount of the wing which verified the calculated lift quite well. We saved the beer for the weekends, when there were women around. (And we were too young for the bars at that time.)
Jackdaw, that was my Junior year, and I think it qualifies as solid working experience of what was really happening. Based on this work, my Professor invited me to write a senior thesis for him based on theoretical work, then instrumenting and running our supersonic wind tunnel to study detailed flow patterns at Mach 2-4.
Jackdaw, that was my Junior year, and I think it qualifies as solid working experience of what was really happening. Based on this work, my Professor invited me to write a senior thesis for him based on theoretical work, then instrumenting and running our supersonic wind tunnel to study detailed flow patterns at Mach 2-4.
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