The influence of leading-edge tubercles on airfoil performance at low Reynolds numbers-Reference-Cited by-同舟云学术

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The influence of leading-edge tubercles on airfoil performance at low Reynolds numbers

Published:2020-01-05 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2020 Forum
language:
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Author:

S Sudhakar¹,L Venkatakrishnan¹,O N Ramesh²

Affiliation:

1. National Aerospace Laboratories

2. Indian Institute of Science

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. Low-Reynolds-Number Airfoils

2. Airfoil boundary layer measurements at low Re in an accelerating flow from a nonzero velocity

3. Laminar separation bubbles and airfoil design at low Reynolds numbers

Cited by 3 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. Effect of aero-shaped vortex generators on NACA 4415 airfoil;Ocean Engineering;2024-01

2. Experimental Investigations on Aerodynamics Parameters of Combined Tubercles with Vortex Generator on NACA 0015 Wing Airfoils;Intelligent Manufacturing and Energy Sustainability;2023-11-28

3. The Effect of Leading-Edge Wavy Shape on the Performance of Small-Scale HAWT Rotors;Energies;2023-09-04

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