Experimental and Theoretical Study on Aeroelastic Response of High-Aspect-Ratio Wings

By D. Tang, Earl H. Dowell. 2001

327 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/5ae3370143265e7fc79442673a1f7bc72d7ddcfd

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Rafael Palacios
2. Paul J. Goulart
3. R. Cook
4. Carlos E. S. Cesnik
5. C. Shearer
6. J. Murua
7. Julia Maria Graham
8. Weihua Su

In Computational Mechanics

1. Rafael Palacios
2. Paul J. Goulart
3. R. Cook
4. Carlos E. S. Cesnik
5. C. Shearer
6. J. Murua
7. Julia Maria Graham
8. Weihua Su

Citations in the corpus

• Nonlinear Flight Dynamics of Very Flexible Aircraft (2005, methodology): “Tang and Dowell [33,34] provided experimental validation of an ONERA unsteady aerodynamic model coupled with nonlinear structural modeling.”
• Robust Gust Alleviation and Stabilization of Very Flexible Aircraft (2013, background): “For high-aspect-ratio aircraft at low velocities (such as typical HALE UAV conditions) two-dimensional (2-D), inviscid, unsteady, aerodynamic models have been shown to predict behavior well [5,6].”