Numerical Investigation of the Flow Field Around Delta Wings
Principal Investigator:
Stefan Hickel
Affiliation:
Institute of Aerodynamics and Fluid Mechanics, Technische Universität München
Local Project ID:
pr47bu
HPC Platform used:
SuperMUC of LRZ
Date published:
Delta wings, or wings with a triangular planform, are an important reference configuration for applied high-performance aerodynamics as well as for basic fluid mechanics studies. They represent tailless aircrafts, so called flying wings, or high-speed high-agility aircrafts with low aspect-ratio wings. Delta wings with smaller dimensions are frequently used for passive flow control (so called vortex generators). The flow around delta wings involves much more complex fluid-flow phenomena than the flow around conventional wings with high aspect ratio. This additional complexity mostly results from strong interactions between lift dependent leading-edge vortices. Detailed turbulence resolving numerical simulations, such as those conducted in this project, are therefore indispensable.
Full report available at: http://inside.hlrs.de/_old/htm/Edition_02_12/article_07.html
Scientific Contact
Dr. Stefan Hickel
Large Eddy Simulation Group, Institute of Aerodynamics and Fluid Mechanics, Technische Universität München
D-85747 Garching bei München
e-mail: sh [@] tum.de
local project ID: pr47bu
September 2013