| 高速飞机总静压探头的气动设计、仿真和测试 |
| Aerodynamic design, Simulation and Experiment of High-speed aircraft Total static pressure probe |
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| 中文摘要: |
| 阐述了高速飞机总静压探头的气动设计、CFD仿真、风洞测试、飞行校测。通过旋成体理论实现总静压探头补偿型面在设计阶段的快速调整，通过商用CFD软件得出静压误差的仿真。设计的总静压探头气动性能需要通过风洞测试的验证，并最终通过飞行校测验证其是否满足使用要求。 |
| 英文摘要: |
| This paper mainly expounds the aerodynamic design, CFD simulation, wind tunnel experiment, flight test of the total static pressure probe in the high-speed aircraft. The compensation surface of the total static pressure probe can be rapidly adjusted in the design phase through revolution body theory. It concludes the simulation of the static pressure through the commercial CFD software. The aerodynamic performance of the total static pressure probe that is designed should be verified through the wind tunnel test, and it should be ultimately verified whether it meets the requirements or not through the flight test. |
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| 中文关键词: 总静压探头 气动设计 CFD 风洞测试 飞行校测 |
| 英文关键词:total static pressure probe, aerodynamic design, CFD, wind tunnel experiment, flight test |
| 基金项目: |
| DOI：10.11823/j.issn.1674-5795.2017.03.08 |
| 引用本文：杜振宇,石岩,张亚军.高速飞机总静压探头的气动设计、仿真和测试[J].计测技术,2017,37(3):42~44. |
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