The characteristics of a Clark y wing model equipped with several forms of low-drag fixed slots (1933)
NASA Technical Reports Server (NTRS) · leaf 5
the The extreme range of angle of attack extended from leading edge. — 6° to +40°, the range for any one combination i 1. Choice of the probable best slot arrangement.— depending on the stalling angle. The tests were made ! The probable best arrangement of the auxiliary airfoil at a dynamic… … - 6.0%c A \ Slot depth = 1.0 per cent chord above main Width wing chord. Figupk 1.—Changes in shape of the auxiliary airfoil Slot width = 6.0 per cent chord. at standard atmospheric conditions. The Reynolds : The location of the auxiliary airfoil with respect to Number based on the above test…
NASA Technical Reports Server (NTRS)
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