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- Investigation of a simple device for preventing separation due to shock and boundary-layer interaction
- Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections
- Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Flutter at very high speeds