Wind-tunnel tests were conducted to determine the influence of rain on the aerodynamic performance of the Wortmann FX63-137 wing at Reynolds numbers 100,000-300,000. Models with aspect ratios of 6 and 4 were tested with normal as well as waxed and soaped surfaces to evaluate wettability effects. Test results showed an improvement of performance at the lowest Reynolds number but general deterioration at higher speeds. The primary effect noted was a decrease in lift at higher angles of attack. A favorable result was the elimination of stall hysteresis, which characterizes the Wortmann's normal performance at low Reynolds numbers. At lower Reynolds numbers, rain appeared to lower drag whereas, at higher speeds, drag generally increased.
The report documents PLUTO (Poisson Laplace U TFI Orthogonal), a three dimensional gridding and smoothing program, which was developed in-house between July 1987 and May 1991. The coding was primarily performed by Capt. David Amdahl and Mr. William Strang of the Aerodynamic Methods Group. This document has been reviewed and approved.
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