aircraft intuitive design (aid)
编者注: this file was selected as matlab central
by interfacing user-friendly aircraft modeling with rapid aerodynamic analysis, this program visually depicts how various design parameters affect the way an airplane flies. a video demonstrating some of the code's capabilities can be found on the mathworks website at .
in addition to built-in, linearized stability approximations that are updated every time the aircraft model is adjusted, the program interfaces with the following software for more advanced analysis:
• digital datcom – u.s. air force
• tornado vortex lattice method – tomas melin (kth royal institute of technology)
• avl (athena vortex lattice method) – mark drela and harold youngren (mit)
this program also gains added functionality from the following open source software:
• datcom plot interpolation functions – prof. glenn greiner and lenny gartenberg (erau, daytona beach, fl)
• avl input/output functions – joseph moster (mathworks file exchange)
• datcomimport – mathworks aerospace toolbox – loads datcom "for006.dat" file
• naca456 – ralph carmichael (pdas) – calculates naca 6-series airfoil ordinates
please refer to the documentation for information regarding how to use the program (help > user's manual)
引用格式
zak lietzau (2023). aircraft intuitive design (aid) (https://www.mathworks.com/matlabcentral/fileexchange/66770-aircraft-intuitive-design-aid), matlab central file exchange. 检索来源 .
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版本 | 已发布 | 发行说明 | |
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1.2.0.0 | updated description
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1.0.0.0 | added link to video in description. |
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