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 31
UJ O 6 … O 2 4 6 8 to 12 14 16 18 20 NACA EM L9E2h cc, deg Figure 11.— The variation of with angle of attack for various model configurations.
NASA Technical Reports Server (NTRS)
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