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Showing 1 to 3 of 3 for “"Body Freedom Flutter"”.

  1. Aeroelastic modeling and flutter control in aircraft with low aspect ratio composite wings

    … plate rigidly attached to a fuselage with rigid-body degrees of freedom. Both quasi-steady and quasi-static aerodynamic strip theories were used to analyze several different flutter mechanisms for a variety of low aspect ratio wing configurations. The most critical flutter mechanism was found to …

    vt Repository record for Aeroelastic modeling and flutter control in aircraft with low aspect ratio composite wings (opens in a new tab)

  2. Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings

    … as large deflections, increased drag, onset of flutter, loss of control authority, etc. Aeroelastic tailoring, internal structural layout design and aerodynamic wing shape morphing are all considered to address these aeroelastic problems through multidisciplinary design, analysis and …

    vt Repository record for Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings (opens in a new tab)

  3. Incorporating Flight Dynamics and Control Criteria in Aircraft Design Optimization

    The NASA Performance Adaptive Aeroelastic Wing (PAAW) project goals include significant reductions in fuel burn, emissions, and noise via efficient aeroelastic design and improvements in propulsion systems. As modern transport airplane designs become increasingly lightweight and incorporate high …

    vt Repository record for Incorporating Flight Dynamics and Control Criteria in Aircraft Design Optimization (opens in a new tab)