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• Investigation of a Two-Step Nozzle in the Langley 11-Inch Hypersonic Tunnel
• An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel
• An Investigation of Four Wings of Square Plan Form at a Mach Number of 6.86 in the Langley 11-Inch Hypersonic Tunnel
• Factors affecting the maximum lift-drag ratio at high supersonic speeds