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Overview of CFD Validation Experiments for Circulation Control Applications at NASA

机译:NASA循环控制应用的CFD验证实验概述

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摘要

Circulation control is a viable active flow control approach that can be used to meet the NASA Subsonic Fixed Wing project's Cruise Efficient Short Take Off and Landing goals. Currently, circulation control systems are primarily designed using empirical methods. However, large uncertainty in our ability to predict circulation control performance has led to the development of advanced CFD methods. This paper provides an overview of a systematic approach to developing CFD tools for basic and advanced circulation control applications. This four-step approach includes "Unit", "Benchmark", "Subsystem", and "Complete System" experiments. The paper emphasizes the ongoing and planned 2-D and 3-D physics orientated experiments with corresponding CFD efforts. Sample data are used to highlight the challenges involved in conducting circulation control computations and experiments.
机译:循环控制是一种可行的主动流量控制方法,可用于满足NASA亚音速固定翼项目的“巡航高效”短距起降目标。当前,循环控制系统主要使用经验方法来设计。但是,我们预测循环控制性能的能力存在很大的不确定性,导致了先进CFD方法的发展。本文概述了为基础和高级循环控制应用开发CFD工具的系统方法。此四步方法包括“单元”,“基准”,“子系统”和“完整系统”实验。本文着重介绍了正在进行的和计划的以2D和3D物理为导向的实验以及相应的CFD努力。样本数据用于突出进行循环控制计算和实验所涉及的挑战。

著录项

  • 来源
  • 会议地点 London(GB);London(GB)
  • 作者单位

    NASA Langley Research Center, Hampton, Virginia, 23681 Flow Physics and Control Branch;

    rnNASA Langley Research Center, Hampton, Virginia, 23681 Flow Physics and Control Branch;

    rnNASA Langley Research Center, Hampton, Virginia, 23681 Flow Physics and Control Branch;

    rnNASA Langley Research Center, Hampton, Virginia, 23681 Configuration Aerodynamics Branch;

    rnNASA Langley Research Center, Hampton, Virginia, 23681 Computational AeroSciences Branch;

    rnNASA Langley Research Center, Hampton, Virginia, 23681 Computational AeroSciences Branch;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 V212.131;
  • 关键词

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