Statistics
RANK
111,000
of 300,763
REPUTATION
0
CONTRIBUTIONS
1 Question
1 Answer
ANSWER ACCEPTANCE
100.0%
VOTES RECEIVED
0
RANK
10,279 of 21,072
REPUTATION
60
AVERAGE RATING
4.00
CONTRIBUTIONS
4 Files
DOWNLOADS
7
ALL TIME DOWNLOADS
443
RANK
of 170,821
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
Question
Elliptic Mesh Generation - Graphics/Ploting help
Hi, I am trying to create a grid like the following: I have two vectors: X and Y coordinates. I need to find a way to add...
5 years ago | 1 answer | 0
1
answerSubmitted
Boeing 737-300 - VLM - panel method
Calculation of Cl(y) and Cp(y) using VLM method.
5 years ago | 2 downloads |
Submitted
NACA 2412 - vortex divsion over the chord
NACA 2412 pressure on the upper and lower surface.
5 years ago | 1 download |
Submitted
NACA 00XX - doublet divison over the chord
NACA 00XX - doublet divison over the chord compard to Abbott & Von Doenhoff book.
5 years ago | 1 download |
Submitted
aeroelastic deformations efficiency - divergence speed
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow condition...
5 years ago | 3 downloads |
Warning: Error updating FunctionLine
try to set an intervel fplot(@(x) exp(x),[-3 0],'b') in your case fplot(p,[0 1])
5 years ago | 0




