Unsteady boundary-layer measurement on oscillating airfoils - Transition and separation phenomena in pitching motion-Reference-Cited by-同舟云学术

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Unsteady boundary-layer measurement on oscillating airfoils - Transition and separation phenomena in pitching motion

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Pascazio M.¹,Autric J.¹,Favier D.¹,Maresca C.¹

Affiliation:

1. CNRS/Aix-Marseille I, Univ.; Aix-Marseille II, Univ., IRPHE/ASI Lab., Marseille, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-35

Reference3 articles.

1. cotO 0 45 90 135180225270315360

2. cot(°) 0 45 90 135180225270315360

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Onset of absolute instability on a pitching aerofoil;Journal of Fluid Mechanics;2024-05-29

2. Experimental study on transition of dynamic airfoil in pitching oscillation;Advances in Aerodynamics;2023-03-14

3. Experimental characterization of an unsteady laminar separation bubble on a pitching wing;Experiments in Fluids;2023-01

4. Experimental Characterization of an Unsteady Laminar Separation Bubble on a Pitching Wing;2022-11-05

5. Numerical investigations on unsteady vortical flows and separation-induced transition over a cycloidal rotor at low Reynolds number;Energy Conversion and Management;2022-08

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