Journals
Publish with us
Publishing partnerships
About us
Blog
International Scholarly Research Notices
Table of Contents
International Scholarly Research Notices
/
2015
/
Article
/
Fig 7
/
Research Article
Computational Investigations on the Effects of Gurney Flap on Airfoil Aerodynamics
Figure 7
Static pressure distributions for different GF heights at AoA = 10
°
.