Investigation of Low-speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing with Leading Edge Swept Back 42 Degrees with and Without High-lift Devices (1949)
NASA Technical Reports Server (NTRS) · leaf 14
Figure 1.— Layout of 42° sweptback ving and aileron details. All dimensions in inches. Wing H area, 32.24; aspect ratio, 4.01. uo
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
