95th step of the wing structural optimization process with the NACA0012 airfoil for zero degees angle of attack
Presented results can be downloaded and visualized as a 3DPDF in Free Adobe Reader
Presentation in PPS format including animations [EN]:
Iryda aero-elastic tests[EN] [PPS]
Cosmoprojector aircraft [EN] [PPS]
Presentation in PDF format [EN]:
Iryda aero-elastic tests[EN] [PDF]
Cosmoprojector aircraft [EN] [PDF]
Short project description [PL]: