Please use this identifier to cite or link to this item:
http://hdl.handle.net/20.500.12358/23322
Title | AN IMPROVED GRAPHICAL VISUALIZATION FOR THE SUBSONIC-STEADY AERODYNAMIC OF DELTA WINGS USING MATLAB |
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Untitled | |
Abstract |
The MATLAB programming language is used to write a generalized computer code to numerically simulate the aerodynamic of a lifting surface using the general vortex-lattice method. This code is used to model the flowfield and predict the aerodynamic loads. The subsonic, steady aerodynamic of a delta wing is used as an example. The powerful graphical tools of MATLAB are used to produce the following: 3-D visualizations of the wakes with/without hidden-line removal, the roll-up of the leading edge wakes, the propagation of the convected vortices, and 3-D pressure distributions. The results obtained in the present work support the physical interpretations of the wing-rock phenomenon and the multi-surface interference previously investigated by many authors; yet with significant improvement on the graphical visualizations. |
Authors | |
Type | Journal Article |
Date | 2004 |
Language | English |
Published in | IUG Journal for Natural and Engineering Studies |
Series | Volume: 12, Number: 1 |
Publisher | الجامعة الإسلامية - غزة |
Citation | |
License | ![]() |
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Files in this item | ||
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247-678-1-PB.pdf | 729.7Kb |