TABULATED PRESSURE COEFFICIENTS AND AERODYNAMIC CHARACTERISTICS MEASURED ON THE WING OF THE BELL X-l AIRPLANE IN AN UNACCELERATED LOW-SPEED STALL, IN PUSHOVERS AT MACH NUMBERS OF 0.83 AND 0.99, AND IN A PULL-UP AT A MACH NUMBER OF 1.16

摘要

Tabulated pressure coefficients and aerodynamic characteristics are presented for six spanwise stations on the left, wing of the Bell X-l research airplane. These data were obtained in an unaccelerated low-speed stall, in push-overs at Mach numbers of approximately 0.83 and 0.99, and in a pull-up at a Mach number of approximately 1.16.