CALCULATION OF THE AERODYNAMIC COEFFICIENTS USING MATLAB®
DOI:
https://doi.org/10.15381/idata.v8i1.6167Keywords:
Aerodynamic profile, Sustentation coefficient, Incidence angle, Attack angle, Wind relative speed.Abstract
The article presents the calculation of aerodynamic coefficients of an airship wing's design: sustentation and moment coefficient applying two methods of integration. As a theoretical part, the fine theory of the aerodynamic profile is used and as a calculation tool the MATLAB software is used, through programs which are presented in their respective files. Besides, the outcome of results reports are presented.
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Copyright (c) 2005 Edgar Ruiz Lizama, Eduardo Raffo Lecca
This work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License.
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