Structural and Aerodynamic Models in Nonlinear Flight Dynamics of Very Flexible Aircraft

By Rafael Palacios, J. Murua, R. Cook. 2010

178 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/cbc2be3c407c877f9b2db9144ea530bf212dfe33

How researchers see this paper

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In Aerospace Engineering

1. Rafael Palacios
2. Julia Maria Graham
3. Paul J. Goulart
4. J. Murua
5. R. Cook

In Computational Mechanics

1. Rafael Palacios
2. Paul J. Goulart
3. Julia Maria Graham
4. R. Cook
5. J. Murua

In Control and Systems Engineering

1. Rafael Palacios
2. Julia Maria Graham
3. Paul J. Goulart
4. J. Murua
5. R. Cook

Citations in the corpus

• Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012, methodology): “The equations of motion are obtained from Hamilton’s principle [17], for which the potential,U, and kinetic, T , energy densities per unit length are first computed as”
• Robust Gust Alleviation and Stabilization of Very Flexible Aircraft (2013, methodology): “[6] compared the strip-theory aerodynamics with the unsteady vortexlattice method, and found that for low-enough reduced frequencies, 2-D aerodynamics with wing-tip corrections (based on steady Received 22 October 2011; revision received 19 June 2012; accepted for publication 20 June 2012; published”