Flight Dynamics of Highly Flexible Flying Wings
By Mayuresh J. Patil, Dewey H. Hodges. 2006
346 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Civil and Structural Engineering, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/0110be8354d5a51d3321374c69241e16c8632bb4
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
- Rafael Palacios
- Julia Maria Graham
- J. Murua
- Carlos E. S. Cesnik
- Weihua Su
- C. Shearer
- Dewey H. Hodges
- R. Cook
In Civil and Structural Engineering
- Rafael Palacios
- Carlos E. S. Cesnik
- Weihua Su
- J. Murua
- Julia Maria Graham
- Dewey H. Hodges
- Wenbin Yu
- Erasmo Carrera
In Control and Systems Engineering
Citations in the corpus
- Nonlinear Flight Dynamics of Very Flexible Aircraft (2005, background): “Patil and Hodges [24], Su and Cesnik [25], and Patil and Taylor [26] studied the nonlinear structural flight dynamics of a flying wing configuration using 1-”
- Dynamic Response of Highly Flexible Flying Wings (2011, methodology): “It is based directly on the vehicle definition presented in [4].”
- Geometrically Exact, Intrinsic Theory for Dynamics of Curved and Twisted Anisotropic Beams (2004, methodology): “Though not applicable to all problems involving beam analysis, they were applied in fully intrinsic form to the aeroelasticity of HALE aircraft in the computer code NATASHA (Nonlinear Aeroelastic Trim and Stability Analysis of HALE Aircraft) [2,3].”
- Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012, methodology): “To address this, the response of such non-conventional aircraft concepts to these disturbances has been studied recently by different authors, including flying-wing configurations [8, 147, 200], blended-wing-body airliners [163], and flexible HALE platforms [134].”