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非定常民用飞机空气动力学的高保真模拟:问题与展望。分区分离涡模拟的应用。

High-fidelity simulations of unsteady civil aircraft aerodynamics: stakes and perspectives. Application of zonal detached eddy simulation.

机构信息

ONERA-The French Aerospace Laboratory, 92190 Meudon, France

ONERA-The French Aerospace Laboratory, 92190 Meudon, France.

出版信息

Philos Trans A Math Phys Eng Sci. 2014 Aug 13;372(2022):20130325. doi: 10.1098/rsta.2013.0325.

Abstract

This paper provides an up-to-date survey of the use of zonal detached eddy simulations (ZDES) for unsteady civil aircraft applications as a reflection on the stakes and perspectives of the use of hybrid methods in the framework of industrial aerodynamics. The issue of zonal or non-zonal treatment of turbulent flows for engineering applications is discussed. The ZDES method used in this article and based on a fluid problem-dependent zonalization is briefly presented. Some recent landmark achievements for conditions all over the flight envelope are presented, including low-speed (aeroacoustics of high-lift devices and landing gear), cruising (engine-airframe interactions), propulsive jets and off-design (transonic buffet and dive manoeuvres) applications. The implications of such results and remaining challenges in a more global framework are further discussed.

摘要

本文提供了对使用分区分离涡模拟(ZDES)进行非定常民用飞机应用的最新调查,以反映混合方法在工业空气动力学框架中的应用的重要性和前景。讨论了用于工程应用的分区或非分区处理湍流的问题。本文使用的基于依赖流场分区的 ZDES 方法进行了简要介绍。介绍了一些最近在整个飞行包线条件下的里程碑式的成就,包括低速(高升力装置和起落架的空气声学,巡航(发动机机体相互作用),推进喷气机和非设计(跨声速抖振和俯冲机动)应用。在更全面的框架中进一步讨论了此类结果的影响和仍然存在的挑战。

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本文引用的文献

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