this repo will be a collection of airfoil analysis codes that automates, facilitates, and accelerate the required analysises of the airfram, including:
- preliminary aerodynamics analysis.
- structure analysis.
- Thrust calculations.
- drag estimations on both laminar and turbulent.
- Fuselage dimensions.
note: the codes will be in the form of both separate functions using matlab, but not limited to, and a final product/form of library
For now, the repo has only has the preliminary aerodynamics analysis as a MATLAB function Ver1.5.
Copyright (C) 2023-2024 AeroSpace_CairoUniversity <[email protected]/[email protected]>
This file is part of the DBF project under Cairo University UDC created by Ahmed Hassan (Main Contributor) and Used by his DBF Team So High In The Sky.
The contributors only in this repository not in the whole community retain all rights to the source code and no one may reproduce, distribute, or create derivative works from this work (All the Repository Codes/libraries/functions).
If you/compony wants to use the Work in this repository, you must meet the following certaain conditions:
- mention Our DBF Team "So High In The Sky" and/or the Main contributor both in text/line citation, in appendix, and acknowledgement (If present) .
- mention The GitHub Community "AeroSpace_CairoUniversity".
- use the code for private and individual cases in your project or competitions only, and after fulfilling points 1 and 2.
- not use in Patent Uses, except if the Main contributor took acknowledgement and a share.
Note: The DBF project under Cairo University UDC project can not be copied and/or distributed without the express permission of {So High In The Sky} <[email protected]/[email protected]>.