Article Dans Une Revue International Journal of Turbo & Jet-Engines Année : 2019

CFD Design Study of a Pressure Probe for Centerline Static Pressure Measurement in Supersonic Ejectors

Résumé

The measurement of the static pressure of the flow inside a supersonic ejector can be achieved by using a thin tube with a radially drilled hole to capture the flow pressure, and which is inserted along the ejector axis. This paper presents a numerical study by CFD permitting to predict the disturbances generated by the presence of the probe in the ejector. Also this study allows guiding the design of the probe, in particular of the capillary tube diameter for the least disturbed measurement. A probe prototype has been built and tested on an ejector test bench.

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Dates et versions

hal-02402878 , version 1 (10-12-2019)

Identifiants

  • HAL Id : hal-02402878 , version 1

Citer

Ala Bouhanguel, Philippe Désévaux, Mohamed Khan. CFD Design Study of a Pressure Probe for Centerline Static Pressure Measurement in Supersonic Ejectors. International Journal of Turbo & Jet-Engines, 2019, 36 (1), pp.107 - 112. ⟨hal-02402878⟩
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