NSERC/Lockheed Martin/Bell Helicopter Industrial Research Chair for Multi-physics Analysis and Design of Aerospace Systems

NSERC/洛克希德·马丁/贝尔直升机航空航天系统多物理分析与设计工业研究主席

• 批准号: 256851-2013
• 负责人: Habashi, Wagdi
• 金额: $ 11.66万
• 依托单位: McGill University
• 依托单位国家: 加拿大
• 项目类别: Industrial Research Chairs
• 财政年份: 2015
• 资助国家: 加拿大
• 起止时间: 2015-01-01 至 2016-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=591583
• 关键词: NSERC; Lockheed; Martin; Bell; Helicopter

Aircraft designers continually strive to optimize aerodynamic efficiency and increase the comfort and safety of air travel. This is addressed by embedding into the design process a complex interplay of disciplines like aerodynamics, structural elasticity and dynamics, as well as safety concerns such as in-flight icing. Such multi-physics numerical approaches, anchored around Computational Fluid Dynamics, have become the most widely used platforms for aircraft design. The objective of the research is to develop new multi-physics computational approaches capable of providing deeper understanding of the interaction between many different phenomena and support the need for accurate and efficient tools for the design of future aircraft. The research will cover topics ranging from hypersonic high-altitude gas dynamics to helicopter aerodynamics and aero-icing, and encompassing the development of efficient meshing tools and advanced Reduced Order Modeling for cost-effective real-time calculations. The research is financed by Lockheed Martin and Bell Helicopter and the outcomes of the research will put the Canadian aerospace sector at the forefront of the scientific and industrial aerospace communities, within the selected fields of research. It is the intention of both companies to increase their research activities in Canada through this Chair, and in the case of LMCO, to establish a new Canadian entity to industrialize the results of this research.

飞机设计师不断努力优化空气动力学效率，并提高飞机的舒适性和安全性。 航空旅行。这是通过在设计过程中嵌入复杂的学科相互作用来解决的， 空气动力学、结构弹性和动力学，以及飞行中结冰等安全问题。等 以计算流体动力学为基础的多物理场数值方法已经成为 广泛用于飞机设计的平台。 该研究的目标是开发新的多物理计算方法， 更深入地了解许多不同现象之间的相互作用，并支持准确的 为未来飞机的设计提供了有效的工具。 这项研究将涵盖从高超音速高空气体动力学到直升机空气动力学等课题 和航空结冰，并包括开发高效的网格工具和先进的降阶 为具有成本效益的实时计算建模。 该研究由洛克希德·马丁公司和贝尔直升机公司资助，研究结果将使 加拿大航空航天部门处于科学和工业航空航天界的前沿， 选定的研究领域。 这是两家公司的意图，以增加他们的研究活动在加拿大通过这个椅子，并在 以LMCO为例，建立一个新的加拿大实体，将这项研究的成果产业化。