通過將使用者友好互動的飛機建模與快速空氣動力學分析相結合，本程式直觀地描述了各種設計引數如何影響飛機的飛行方式。

By interfacing user-friendly aircraftmodeling with rapid aerodynamic analysis, this program visually depicts howvarious design parameters affect the way an airplane flies.

MathWorks網站上驗證該程式碼的視訊網址如下：

除了在調整飛機模型時更新的內建線性穩定近似值之外，程式還支援與下列軟體進行介面，以便進行更高階的分析：

In addition to built-in, linearizedstability approximations that are updated every time the aircraft model isadjusted, the program interfaces with the following software for more advancedanalysis:

1. Digital DATCOM –U.S.Air Force 
   

2. Tornado Vortex Lattice Method –Tomas Melin (KTH Royal Institute of Technology) 
    
   

3. AVL (Athena Vortex LatticeMethod) – Mark Drela and Harold Youngren (MIT)
   

本程式碼還可以通過以下開源軟體獲得附加的其它功能：

1. DATCOM Plot InterpolationFunctions – Prof. Glenn Greiner and Lenny Gartenberg (ERAU, Daytona Beach, FL) 
   

2. AVL Input/Output Functions –Joseph Moster (Mathworks File Exchange) 
   

3. Datcomimport – MathWorksAerospace Toolbox – loads DATCOM "for006.dat" file 
    
   

4. NACA456 – Ralph Carmichael(PDAS) – calculates NACA 6-series airfoil ordinates
   

工具箱外掛下載地址：

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