Flight measurements of the pressure distribution on the wing of the X-1 airplane (10 percent thick wing) over a chordwise station near the midspan, in level flight at Mach numbers from 0.79 to 1.00 and in a pull up at a Mach number of 0.98
Description: Report presenting measurements of chordwise pressure distribution over the 10-percent-thick wing of the X-1 research airplane at a section near the midspan of the left wing. Results regarding the upper- and lower-surface pressure distributions at a range of Mach numbers and section loads are provided.
Date: September 12, 1950
Creator: Carner, H. Arthur & Knapp, Ronald J.
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Partner: UNT Libraries Government Documents Department