Summary
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 flow around transport aircraft high lift configurations based on the solution of the Reynolds-averaged Navier-Stokes equations. The project NHLRes II, a follow-on activity of the NHLRes project [1], consists of three parts representing a analysis of complex 3D-flow features, wake vortex simulations and an optimization task for selected three-dimensional high lift flow problems.
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Melber-Wilkending, S., Stumpf, E., Wild, J., Rudnik, R. (2003). Numerical High Lift Research II. In: Krause, E., Jäger, W., Resch, M. (eds) High Performance Computing in Science and Engineering ’03. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-55876-4_24
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DOI: https://doi.org/10.1007/978-3-642-55876-4_24
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