he control desk in the test representing approximately the location of the wings chamber. The other side of the manometer is left open of an airplane during tests was most completely to the test-chamber pressure. This installation has explored. The dynamic-pressure distribution over the been… … FiGTOR 6.—A 6 by 36 foot Clark Y sirfoU monnted in the tunnel. location and it is used to determine the dynamic head of a mean value. It is possible to improve the distri- during tests. bution by further adjustment of the guide vanes. A series of Clark T airfoils of the same aspect ratio, However,…
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