Statistics
File Exchange
1 File
RANK
N/A
of 300,967
REPUTATION
N/A
CONTRIBUTIONS
0 Questions
0 Answers
ANSWER ACCEPTANCE
0.00%
VOTES RECEIVED
0
RANK
7,113 of 21,126
REPUTATION
147
AVERAGE RATING
4.50
CONTRIBUTIONS
1 File
DOWNLOADS
5
ALL TIME DOWNLOADS
1383
RANK
of 172,078
CONTRIBUTIONS
0 Problems
0 Solutions
SCORE
0
NUMBER OF BADGES
0
CONTRIBUTIONS
0 Posts
CONTRIBUTIONS
0 Public Channels
AVERAGE RATING
CONTRIBUTIONS
0 Discussions
AVERAGE NO. OF LIKES
Feeds
Submitted
Novel Implementation of Hess and Smith panel method using Data structures
Code to plot pressure variation on NACA 4 digit aerofoil and calculate lift variation
13 years ago | 5 downloads |
