The effect of undulating leading-edge modifications on NACA 0021 airfoil characteristics-Reference-Cited by-同舟云学术

The effect of undulating leading-edge modifications on NACA 0021 airfoil characteristics

Published:2013-11 Issue:11 Volume:25 Page:117101
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Rostamzadeh N.,Kelso R. M.,Dally B. B.,Hansen K. L.

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/10.1063/1.4828703

Reference19 articles.

1. Validating the URANS shear stress transport γ −Reθ model for low-Reynolds-number external aerodynamics

2. D. Custodio, “The effect of humpback whale-like leading edge protuberances on hydrofoil performance,” Ph.D. thesis, Worcester Polytechnic Institute, December 2007.

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