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Description of the test cases

Author
Bugeda, G.; Périaux, J.; Qin, N.; Pons-Prats, J.
Type of activity
Book chapter
Book
Advances in effective flow separation control for aircraft drag reduction: modeling, simulations and experimentations
First page
27
Last page
53
Publisher
Springer
Date of publication
2020
ISBN
978-3-030-29687-2 Open in new window
DOI
10.1007/978-3-030-29688-9
Repository
http://hdl.handle.net/2117/174787 Open in new window
http://hdl.handle.net/2117/174790 Open in new window
URL
https://link.springer.com/book/10.1007%2F978-3-030-29688-9 Open in new window
Abstract
The high-level objective of MARS project was to understand the formation and behaviour of turbulent structures which affects the Reynolds stress and skin friction. The aim was, once understood, to apply flow control techniques in order to control these structures and reduce the overall drag derived from the Reynolds stress and mainly from the skin friction. Active flow control devices were the main interest; DBD plasma, Synthetic jets, Micro Blowing and Suction, Moving Surfaces were included on ...
Citation
Bugeda, G. [et al.]. Description of the test cases. A: "Advances in effective flow separation control for aircraft drag reduction: modeling, simulations and experimentations". Berlín: Springer, 2020, p. 27-53.
Keywords
Backward facing step, Blowing and suction · Slots, DBD plasma, Drag reduction, Flow control, Fluidric Vortex Generator, MARS, Moving Surface, NACA0015, Reynolds stress, Separation control, Skin friction, Synthetic Vortex Generator, Synthetic jets
Group of research
(MC)2 - UPC Computational continuum mechanics
GMNE - Numerical Methods in Engineering Group
RMEE - Strength of Materials and Structural Engineering Research Group

Participants