Unsteady Behavior of a Laminar Separation Bubble Subjected to Wing Structural Motion
Author:
Affiliation:
1. Technische Universiteit Delft Faculteit Luchtvaart- en Ruimtevaarttechniek
2. The University of Arizona
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2331
Reference44 articles.
1. Horton, H. "Laminar Separation Bubbles in Two and Three Dimensional Incompressible Flow," Ph.D. thesis,University of London, 1968.
2. Evolution of a wave packet into vortex loops in a laminar separation bubble
3. Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV
4. High-fidelity simulations of moving and flexible airfoils at low Reynolds numbers
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1. High-Order-Accurate Incompressible Flow Solver for High-Fidelity Numerical Simulations and Linear Stability Analysis;AIAA Journal;2023-04
2. Experimental characterization of an unsteady laminar separation bubble on a pitching wing;Experiments in Fluids;2023-01
3. Experimental Characterization of an Unsteady Laminar Separation Bubble on a Pitching Wing;2022-11-05
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