<script type="text/javascript">
<!--
document.write('<div id="oa_widget"></div>');
document.write('<script type="text/javascript" src="https://beta.openaire.eu/index.php?option=com_openaire&view=widget&format=raw&projectId=undefined&type=result"></script>');
-->
</script>

COPY SCRIPT

For further information contact us at helpdesk@openaire.eu

Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap

descriptionPublicationkeyboard_double_arrow_right Article , Journal , Other literature type 01 Dec 2020 Germany, Switzerland Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:AIAA Journal, volume 58, pages 5,146-5,155 (issn: 0001-1452, eissn: 1533-385X,

Authors: He, Guosheng; Deparday, Julien; Siegel, Lars; Henning, Arne; Mulleners, Karen;

doi: 10.2514/1.j059719

Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap

- Summary
- Subjects
- Metrics

Abstract

The flow around a pitching NACA0015 airfoil with an oscillating trailing-edge flap is experimentally investigated to characterize the influence of the flap kinematics on the development of dynamic ...

Countries

Germany, Switzerland

Related Organizations

École Polytechnique Fédérale de Lausanne EPFL
Switzerland
German Aerospace Center
Germany

Keywords

trailing-edge flap, pitching airfoil, pressure measurements, particle image velocimetry, dynamic stall

Impact byBIP!

	citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	19
	popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.	Top 10%
	influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	Top 10%
	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Top 10%

Found an issue? Give us feedback

Top 10%

Fields of Science

Fields of Science

Funded by

SNSF| Dynamic stall management for improving aerodynamic robustness of H-type wind turbine, DFG| unidentified

Related to Research communities

Energy Research