Measurements of the chordwise pressure distributions over the wing of the XS-1 research airplane in flight
Description:
Report presenting measurements of the chordwise pressure distributions over the 8-percent-thick wing of the XS-1 research airplane at a section near the midspan of the left wing. Data are presented for a Mach number range and a normal-force coefficient of about 0.33. Results regarding the upper-surface pressure distribution, lower-surface pressure distributions, and total section loads are provided.
Date:
August 4, 1948
Creator:
Beeler, De E.; McLaughlin, Milton D. & Clift, Dorothy C.
Partner:
UNT Libraries Government Documents Department