首页> 外文期刊>AIAA Journal >Numerical Study of Transitional SD7003 Airfoil Interacting with Canonical Upstream Flow Disturbances
【24h】

Numerical Study of Transitional SD7003 Airfoil Interacting with Canonical Upstream Flow Disturbances

机译:SD7003翼型与典型上游扰动相互作用的数值研究

获取原文
获取原文并翻译 | 示例
           

摘要

The current work reports on the results of high-accuracy two-dimensional and high-fidelity three-dimensional Navier-Stokes simulations of an SD7003 airfoil interacting with canonical upstream flow disturbances at low and moderate Reynolds numbers corresponding to laminar and transitional flow regimes. Three deterministic forms of upstream flow disturbances are considered, including sharp-edge gust, time-harmonic gust, and Taylor vortex models. The results obtained for the airfoil unsteady aerodynamic responses to gust perturbationswith variable amplitude and duration are discussed in comparison with results from linearized inviscid incompressible unsteady aerodynamic theory to elucidate the importance of viscous effects in the considered flow regimes. Overall, the investigation reveals that the high-amplitude gust responses correlate well with inviscid theories, which is in contrast to the low-amplitude gust responses that appear to be strongly affected by viscous effects.
机译:当前的工作报告了SD7003翼型在与层流和过渡流态相对应的中低雷诺数下与规范的上游流动扰动相互作用的高精度二维和高保真度Navier-Stokes模拟结果。考虑了三种确定性形式的上游流动扰动,包括尖锐阵风,时谐阵风和泰勒涡模型。与线性无粘性不可压缩非稳态空气动力学理论的结果相比较,讨论了机翼对阵风扰动具有可变幅度和持续时间的非稳态空气动力学响应的结果,以阐明粘性效应在考虑的流动状态下的重要性。总的来说,研究表明,高振幅阵风反应与无粘性理论具有很好的相关性,而低振幅阵风反应似乎受到粘性作用的强烈影响。

著录项

  • 来源
    《AIAA Journal》 |2018年第1期|158-181|共24页
  • 作者单位

    Embry Riddle Aeronaut Univ, Dept Aerosp Engn, Daytona Beach, FL 32114 USA;

    Embry Riddle Aeronaut Univ, Dept Aerosp Engn, Daytona Beach, FL 32114 USA;

    US Air Force, Res Lab, Wright Patterson AFB, OH 45433 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号