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

Wind Tunnel Testing of High-Rise Buildings

Peter Irwin

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

KC-135 Winglet Program Review

KC-135 Winglet Program Review (1981 Edwards, Calif.)

Langley 8-ft. HTT test 139 gas analyses

Danny R. Sprinkle

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

Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results

L. Tracy Redd