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by Ronald H. Soeder
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Slotted-wall flow-field measurements in a transonic wind tunnel
Joel L. Everhart
Assessment of dual-point drag reduction for an executive-jet modified airfoil section
Dennis O. Allison
The NASA Langley 8-foot transonic pressure tunnel calibration
Cuyler W. Brooks
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
Julio Chu
Control of the NASA Langley 16-foot transonic tunnel with the self-organizing feature map
Mark A. Motter
Computation of imaginary-side pressure distributions over the flexible walls of the test section insert for the 0.3-M transonic cryogenic tunnel
M. J. Goodyer
Evaluation of flow quality in two large NASA wind tunnels at transonic speeds
Bill Harvey
Demonstration of imaging flow diagnostics using Rayleigh scattering in Langley 0.3-Meter Transonic Cryogenic Tunnel
B. Shirinzadeh
Simulation of ideal-gas flow by nitrogen and other selected gases at cyogenic temperatures
Robert M. Hall