Pressure Measurements on Five Miniature Mach/Flow Angularity Probes at Mach Numbers 1.76, 2.0, 3.0 and 5.0
Final rept. for the period ending 20 Mar 1983
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
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Pressure measurements were obtained on five miniature Machflow angularity MFA probes which were developed at AEDC as part of an on-going probe development effort. These measurements will be correlated with Mach number and known flow angle in order to calibrate these probes. Secondary objectives were to test a hot-film anemometer and three pitot acoustic probes for durability, and to examine the response of three ported dynamic pressure transducers located downstream of the tunnel test section.
- Test Facilities, Equipment and Methods
- Fluid Mechanics