Turbulence Measurement in Hypersonic Flow,
COMPLERE INC PALO ALTO CA
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An assessment has been made of the potential for hot wire and laser anemometer measurements of turbulent fluctuations in hypersonic flow fields. The results of experiments conducted in the AFWAL M6 High Reynolds Number Wind Tunnel are reported and comparisons made with previous hot wire turbulence measurements.
- Fluid Mechanics
- Test Facilities, Equipment and Methods