aircraft intuitive design (aid) -凯发k8网页登录

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)