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Investigation of Air Flow in Right-Angle Elbows in a Rectangular Duct

Investigation of a Two-Step Nozzle in an 11-Inch Hypersonic Tunnel

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


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