EXPERIMENTAL INVESTIGATION OF THE SURFACE IMPACT PRESSURE PROBE METHOD OF MEASURING LOCAL SKIN FRICTION AT SUPERSONIC SPEEDS.
DEFENSE RESEARCH LAB UNIV OF TEXAS AUSTIN
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The purpose of the report is to demonstrate, on the basis of wind tunnel results, the feasibility of using a surface probe. This phase is limited to thermally insulated surfaces with zero pressure gradient.
- Test Facilities, Equipment and Methods
- Fluid Mechanics