N.T.U.A. animation Titles picture Animation


Examples of Data Visualization using Se.La.Vi.

Title : Calculation of the flow around BO105 helicopter model
Flow calculations performed by : Dimitris Triantos
Description :

The calculation were performed with unsteady vortex
particle method. For the case of the BO105 helicopter
model, there were used 1536 panels to simulate the geometry
(main rotor, tail rotor and fuselage) the full developed wake
were consider from 54000 vortex particles.
Calculation conditions : 
forward flight speed 32.75 m/sec
the main rotor is hingeless with cyclic pitch control

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zip file 2.9 MB includes avi file , 640x480 ,
450frames , 50 sec , original size 8.7 MB



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