Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

Thomas A. Byrdsong

1983

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Wind Tunnel Testing of High-Rise Buildings

Peter Irwin

2013

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Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊

Emma Jean Landrum

1977

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Langley 8-ft. HTT test 139 gas analyses

Danny R. Sprinkle

1999

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Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊

Emma Jean Landrum

1979

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