Numerical Investigation on the Reynolds Number Effects of Supercritical Airfoil-Reference-Cited by-同舟云学术

Numerical Investigation on the Reynolds Number Effects of Supercritical Airfoil

Published:2012 Issue: Volume:31 Page:103-109
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Liu Dawei,Wang Yuanjing,Chen Dehua,Peng Xin,Xu Xing

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference4 articles.

1. Dawei LIU; Dehua CHEN; Yuanjing WANG: Reynolds Number Effect Investigation of Supercritical Airfoil Based on Wind Tunnel Test. System Simulation Technology & Application(Volume 13), 2011.

2. R.W. Clark and R. A. Pelkman High Reynolds Number Testing of Advanced Transport Aircraft Wings in the National Transonic Facility. AIAA-2001-0910.

3. CHEN Zuobing: Computational Fluid Dynamics and application. National Defense Industrial Press. 2001.

4. L. Wayne McKinney: Wind-Tunnel/Flight Correlation-1981. NASA Conference Publication 2225.

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