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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

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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.

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Available 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.

Key concepts: Pitot tube, Mach number, Anemometer, Flow (mathematics), Mach wave, Acoustics, Mechanics, Pressure measurement

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Pressure Measurements on Five Miniature Mach/Flow Angularity Probes at Mach Numbers 1.76, 2.0, 3.0 and 5.0 — Research Paper | ScholarLens