Numerical high lift research - NHLRes annual review 2001

被引：0

作者：

Melber, S ^{[1
]}

Wild, J ^{[1
]}

Rudnik, R ^{[1
]}

机构：

[1] DLR, Inst Aerodynam & Flor Technol, Sect Transport Aircraft, D-38108 Braunschweig, Germany

来源：

HIGH PERFORMANCE COMPUTING IN SCIENCE AND ENGINEERING '02 | 2003年

关键词：

D O I：

暂无

中图分类号：

TP301 [理论、方法];

学科分类号：

081202 ;

摘要：

The project NHLRes is concerned with the simulation of aircraft aerodynamics and thus belongs to the research field of computational fluid dynamics (CFD) for aerospace applications. NHLRes comprises the numerical simulation of the viscous compressible flow around transport aircraft high lift configurations. The investigations are based on the solution of the Reynolds-averaged Navier-Stokes equations using a finite volume parallel solution algorithm with an unstructured data concept. The project consists of two parts representing a typical analysis as well as an optimization task for selected three-dimensional high lift flow problems.

引用

页码：406 / 421

页数：16

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