On the onset of negative lift in a symmetric airfoil at very small angles of attack-Reference-Cited by-同舟云学术

On the onset of negative lift in a symmetric airfoil at very small angles of attack

Published:2020-05-01 Issue:5 Volume:32 Page:055107
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Aguilar-Cabello Jorge¹^ORCID,Gutierrez-Castillo Paloma¹^ORCID,Parras Luis¹^ORCID,del Pino Carlos¹^ORCID,Sanmiguel-Rojas Enrique¹

Affiliation:

1. Escuela de Ingenierías Industriales, Universidad de Málaga, Campus de Teatinos, 29071 Málaga, Spain

Funder

Ministerio de Economia y Competitividad

Junta de Andalucia

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0008348

Reference37 articles.

1. Low-Reynolds-Number Airfoils

2. E. N. Jacobs, K. E. Ward, and R. M. Pinkerton, “The characteristics of 78 related airfoil sections for tests in the variable-density wind tunnel,” Report No. 460, National Advisory Committe for Aeronautis (NACA), 1935.

3. Control of flow around a NACA 0012 airfoil with a micro-riblet film

4. Modification of a wing tip vortex by vortex generators

5. Feedback flow control of a low-Re airfoil by flap actuators

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