Numerical Simulation Research on Pressure Probe

DOI

10.2991/masta-19.2019.52How to use a DOI?

Keywords

Complex probe, Transonic flow, Numerical simulation

Abstract

This article presents an investigation on the flow characteristics of the air in complex probe. The flow fields around the complex probe in different Mach numbers is simulated to analysis the relation between flow field structure and text parameters. The investigation on complex probe shows that the Mach numbers has influence on the characteristic of complex probe. The flow field around the probe and shock wave distribution transform with the change of Mach number. The calibrate coefficient has disparate transformation law in subsonic speed flow field, near-sonic speed flow field and supersonic speed flow field.

Copyright

© 2019, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yi Zhang
AU  - Yu-bin Men
PY  - 2019/07
DA  - 2019/07
TI  - Numerical Simulation Research on Pressure Probe
BT  - Proceedings of the 2019 International Conference on Modeling, Analysis, Simulation Technologies and Applications (MASTA 2019)
PB  - Atlantis Press
SP  - 310
EP  - 314
SN  - 1951-6851
UR  - https://doi.org/10.2991/masta-19.2019.52
DO  - 10.2991/masta-19.2019.52
ID  - Zhang2019/07
ER  -