Development of high level application programming interface for heterogeneous computing systems for low-fidelity aerodynamic codes

为低保真空气动力学代码的异构计算系统开发高级应用程序编程接口

• 批准号: 461419-2013
• 负责人: Laurendeau, Eric
• 金额: $ 1.82万
• 依托单位: École Polytechnique de Montréal
• 依托单位国家: 加拿大
• 项目类别: Engage Grants Program
• 财政年份: 2013
• 资助国家: 加拿大
• 起止时间: 2013-01-01 至 2014-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=542615
• 关键词: Development; level; application; programming; interface

Aerospace industry has seen a thriving evolution in the recent decades driven by the demand for delivering ever greener, safer and more economical airplanes. This progress was made possible in part by the integration of Computational Fluid Dynamics (CFD) simulations within the aircraft development process. It limits costly wind-tunnel tests and proves to be reliable for aerodynamic calculations, simultaneously reducing turnaround time and program development risks. Its success stems to a large extent from a tremendous increase of speed of central processing units (CPUs). It is the increase of the computational horsepower of tomorrow's computing architectures that will shape the future of CFD within the aerospace industry. As a response to possible limitations in the further development of CPU architectures, heterogeneous computing systems were

近几十年来，航空航天工业经历了蓬勃发展，这是由于对提供更环保，更安全，更经济的飞机的需求。这一进展部分是由于在飞机开发过程中集成了计算流体动力学（CFD）模拟。它限制了昂贵的风洞试验，并被证明是可靠的空气动力学计算，同时减少了周转时间和程序开发风险。它的成功在很大程度上源于中央处理器（CPU）速度的巨大提高。未来计算架构的计算能力的增加将塑造航空航天工业中CFD的未来。作为对CPU体系结构的进一步发展中可能的限制的响应，