Design modification of airfoil by integrating sinusoidal leading edge and dimpled surface-Reference-Cited by-同舟云学术

Design modification of airfoil by integrating sinusoidal leading edge and dimpled surface

Published:2017 Issue: Volume: Page:
ISSN:0094-243X
Container-title:AIP Conference Proceedings
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Author:

Masud M. H.,Naim-Ul-Hasan ,Arefin Amit Md. Estiaque,Joardder Mohammad U. H.

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Author(s)

Link

http://aip.scitation.org/doi/pdf/10.1063/1.4984677

Reference10 articles.

1. Turbulence modeling of deep dynamic stall at relatively low Reynolds number

2. High-order simulations of low Reynolds number membrane airfoils under prescribed motion

3. P. Watts and F. E. Fish, “The influence of passive, leading edge tubercles on wing performance,” in Proc. Twelfth Intl. Symp. Unmanned Untethered Submers. Technol, 2001.

4. Numerical Analysis of Effects of Leading-Edge Protuberances on Aircraft Wing Performance

5. Drag reduction in flow over a two-dimensional bluff body with a blunt trailing edge using a new passive device

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