Numerical simulation of 'X-wing' type biplane flapping wings in 3D using the Immersed Boundary Method (IBM)
Conference Paper
(2013)
Author(s)
W. Tay (TU Delft - Aerodynamics)
BW van Oudheusden (TU Delft - Aerodynamics)
H Bijl (TU Delft - Aerodynamics)
Research Group
Aerodynamics
To reference this document use:
https://resolver.tudelft.nl/uuid:45065dbb-326e-4a50-82bf-c4122cdf1f44
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Publication Year
2013
Language
English
Research Group
Aerodynamics
Pages (from-to)
85-87
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