Computational study of vortex shedding and its effects on asymmetrical airfoil with gurney flap-Reference-Cited by-同舟云学术

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Computational study of vortex shedding and its effects on asymmetrical airfoil with gurney flap

Published:2024-11 Issue: Volume:24 Page:100796
ISSN:2666-2027
Container-title:International Journal of Thermofluids
language:en
Short-container-title:International Journal of Thermofluids

Author:

Mandal Balram^ORCID,Gupta Roshani Kumari,Adhikari Abhinav,Sheth Mit Manojbhai,Bhoraniya Rameshkumar,Harichandan Atal Bihari

Publisher

Elsevier BV

Reference8 articles.

1. Aerodynamics of gurney flaps on a single-element high-lift wing;Jeffrey;J. Aircr,2000

2. Time resolved PIV analysis of flow over a NACA 0015 airfoil with gurney flap;Troolin;Exp. Fluids,2006

3. Investigation of aeroacoustics and flow dynamics of a NACA 0015 airfoil with a gurney flap using TR-PIV;Shah,2016

4. Examination of gurney flap pressure and shedding characteristics;Traub;J. Aircr,2017

5. Aeroacoustics analysis of an airfoil with Gurney flap based on time-resolved particle image velocimetry measurements;Zhang;J. Sound Vib,2018

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