Wall modeled large eddy simulation of the VFE-2 delta wing
Conference Paper
(2018)
Author(s)
C Zwerger (Technische Universität München)
S Hickel (Technische Universität München, PSA3: Pieter Sijtsma Advanced AeroAcoustics, TU Delft - Aerodynamics)
C Breitsamter (Technische Universität München)
N Adams (Technische Universität München)
Research Group
Aerodynamics
DOI related publication
https://doi.org/10.1007/978-3-319-63212-4_36
To reference this document use:
https://resolver.tudelft.nl/uuid:e814ea8a-d3fd-4fad-a9e7-18d214816d07
More Info
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Publication Year
2018
Language
English
Research Group
Aerodynamics
Volume number
24
Pages (from-to)
289-295
ISBN (print)
978-3-319-63211-7
ISBN (electronic)
978-3-319-63212-4
Abstract
Delta wing configurations are commonly employed for high agility supersonic aircraft and aerodynamic devices such as vortex generators, and have thus been a focus of extensive investigations over the past decades.
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