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by Abbas Khavaran
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A 3-component laser-doppler velocimeter data acquisition and reduction system
L. C. Rodman
A new algorithm for five-hole probe calibration, data reduction, and uncertainty analysis
Bruce A. Reichert
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
Stephen W. D. Wolf
Single-shot spectrally resolved UV Rayleigh scattering measurements in high speed flow
Richard G. Seasholtz
Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel
Jose C. Gonsalez
Supersonic quiet-tunnel development for laminar-turbulent transition research
Steven P. Schneider
Comparison of the aeroacoustics of two small-scale supersonic inlets
Wing Ng
Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer
W. W. Koziak
Experimental measurement of structural power flow on an aircraft fuselage
J. M. Cuschieri
