Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability
Description:
"The pressure distribution data discussed in this report represents the results of part of an investigation conducted on the factors affecting the aerodynamic safety of airplanes. The present tests were made on semispan, circular-tipped Clark Y airfoil models mounted in the conventional manner on a separation plane. Pressure readings were made simultaneously at all test orifices at each of 20 angles of attack between -8 degrees and +90 degrees. The results of the tests on each wing arrangement …
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Date:
October 15, 1931
Creator:
Noyes, Richard W.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department