Computational Aerodynamics for Aircraft Drag Reduction

飞机减阻的计算空气动力学

• 批准号: RGPIN-2017-06760
• 负责人: Zingg, David
• 金额: $ 4.81万
• 依托单位: University of Toronto
• 依托单位国家: 加拿大
• 项目类别: Discovery Grants Program - Individual
• 财政年份: 2017
• 资助国家: 加拿大
• 起止时间: 2017-01-01 至 2018-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=638815
• 关键词: Computational; Aerodynamics; Aircraft; Drag; Reduction

Motivated by the need to reduce the drag of transport aircraft and as a result their CO2 emissions, the proposed research program comprises algorithm development for computational fluid dynamics, algorithm development for aerodynamic shape optimization, and application to drag reduction via unconventional aircraft configurations and active flow control.

由于需要减少运输机的阻力，并因此减少其二氧化碳排放量，建议的研究计划包括计算流体动力学的算法开发，气动外形优化的算法开发，以及通过非常规飞机配置和主动流控制来减少阻力的应用。