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“Think of an airplane as a great body with its end structures (wings, horizontal tail surfaces, vertical tail surfaces) that could have the possibility to change their shape as they had internal nerve endings and muscles ...”
FSI results: deformed fluid dynamic grid of the reference piezo-wing section FSI results: deformed fluid dynamic grid of the reference aileron-wing section A comparison of Cl-Cd curves for the examined wing sections ( h = 0 m, M = 0.17 ) Comparison between Cl-Cd curves for the examined wing sections ( h = 0 m, M = 0.17 )
FSI results: deformed fluid dynamic grid of the reference aileron-wing section (δa=15° - Case 6 of Table 2.6, h=0 m, αg = 2 deg, M=0.17)
FSI results: deformed fluid dynamic grid of the reference piezo-wing section (V/V*=5 - Case 5 of Table 2.5, h=0 m, αg = 2 deg, M=0.17)
Comparison of Cl-Cd curves for the examined wing sections ( h = 0 m, M = 0.17 )
Comparison of Cl-Cd curves for the examined wing sections ( h = 0 m, M = 0.17 )
TOPIC 2 Aeroelastic analysis
Geometry and numerical model of a piezo-controlled and a standard 2D wing section (page 4 of 4)
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