Science and Education Publishing
From Scientific Research to Knowledge
Submission
Browse by Subjects
Search
Journal Home
For Authors
Online Submission
Current Issue
Archive
About Us
Figure 4.
Pressure coefficient distribution for NACA0012 in angle of attack α
0
=6
From
Boundary Element Method Applied to the 2D Foil with Oscillating Heave and Pitch Motions
Mehdi Pourmostafa, Hassan Ghassemi, Parviz Ghadimi
American Journal of Mechanical Engineering
.
2020
, 8(1), 17-25 doi:10.12691/ajme-8-1-3
Previous
Figure
4
of 18 (
Figures index
)
Next