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Aircraft

  
 
Results: Displaying 8 of 88 on page 9 of 9
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Name
Title
Area
Document
Colleges
Year
Attitude control system for fixed SLV model with 3 degree of freedom
Experimental model for Flutter tests of a typical aeroelastic section
Wind tunnel testing of porous devices for the reduction of flap side-edge noise in...
Characterization and detection of freeplay nonlinearity in aeroelastic systems
Aeroelastic state space reconstruction by singular value decomposition
Study of aeronautic hybrid mechanical joints (metal-composite)
Aeronautical interior structures in natural composite: manufacturing, structural...
Energy harvesting study of nonlinear oscillation induced by the flow in a finite...
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Results: Displaying 8 of 88 on page 9 of 9
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