Statistics
1 File
RANK
N/A
of 290,021
REPUTATION
N/A
CONTRIBUTIONS
0 Questions
0 Answers
ANSWER ACCEPTANCE
0.00%
VOTES RECEIVED
0
RANK
7,051 of 19,621
REPUTATION
139
AVERAGE RATING
4.50
CONTRIBUTIONS
1 File
DOWNLOADS
10
ALL TIME DOWNLOADS
1305
RANK
of 144,421
CONTRIBUTIONS
0 Problems
0 Solutions
SCORE
0
NUMBER OF BADGES
0
CONTRIBUTIONS
0 Posts
CONTRIBUTIONS
0 Public Channels
AVERAGE RATING
CONTRIBUTIONS
0 Highlights
AVERAGE NO. OF LIKES
Your submissions were downloaded 30 or more times in a month
Awarded to ronak gupta on 01 Jan 2023
Your submissions received 1 five star rating
Awarded to ronak gupta on 09 Oct 2019
Publish your first submission
Awarded to ronak gupta on 09 Oct 2019
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
11 years ago | 10 downloads |
You can also select a web site from the following list
Americas
- América Latina (Español)
- Canada (English)
- United States (English)
Europe
- Belgium (English)
- Denmark (English)
- Deutschland (Deutsch)
- España (Español)
- Finland (English)
- France (Français)
- Ireland (English)
- Italia (Italiano)
- Luxembourg (English)
- Netherlands (English)
- Norway (English)
- Österreich (Deutsch)
- Portugal (English)
- Sweden (English)
- Switzerland
- United Kingdom (English)
Asia Pacific
- Australia (English)
- India (English)
- New Zealand (English)
- 中国
- 日本Japanese (日本語)
- 한국Korean (한국어)