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美国政府科技报告
>Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the Douglas D-558-I airplane for a 1 g stall, a speed run to a Mach number of 0.90, and a wind-up turn at a Mach number of 0.86
【24h】
Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the Douglas D-558-I airplane for a 1 g stall, a speed run to a Mach number of 0.90, and a wind-up turn at a Mach number of 0.86
