Optimization of SD7003 airfoil performance using TBL and CBL at low Reynolds numbers-Reference-Cited by-同舟云学术

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Optimization of SD7003 airfoil performance using TBL and CBL at low Reynolds numbers

Published:2018-08 Issue: Volume:79 Page:199-211
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kamari Dj.^ORCID,Tadjfar M.,Madadi A.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Active separation control: an overview of Reynolds and Mach numbers effects;Seifert;Aerosp. Sci. Technol.,2004

2. Control of a decelerating boundary layer, part 1: optimization of passive vortex generators;Godard;Aerosp. Sci. Technol.,2006

3. Control of a decelerating boundary layer, part 2: optimization of slotted jets vortex generators;Godard;Aerosp. Sci. Technol.,2006

4. Control of a decelerating boundary layer, part 3: optimization of round jets vortex generators;Godard;Aerosp. Sci. Technol.,2006

5. Time-resolved and volumetric PIV measurements of a transitional separation bubble on an SD7003 airfoil;Burgmann;Exp. Fluids,2008

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