Pressure Measurements on Five Miniature Mach/Flow Angularity Probes at Mach Numbers 1.76, 2.0, 3.0 and 5.0
M. T. Byers, Edward Marquart, J. C. Donaldson, S. STEPANEK
Abstract
M. T. Byers, Edward Marquart, J. C. Donaldson, S. STEPANEK
Abstract
Abstract : Pressure measurements were obtained on five miniature Mach/flow 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.
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Abstract : Pressure measurements were obtained on five miniature Mach/flow 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.
Key concepts: Pitot tube, Mach number, Anemometer, Flow (mathematics), Mach wave, Acoustics, Mechanics, Pressure measurement