Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions
By Philippe Geuzaine, G. Brown, C. Harris, Charbel Farhat. 2003
208 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/2a9eb99c6514802863f4b0c019d0da0dc3cf4d0d
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
- Philip Avery
- Charbel Farhat
- Julia Maria Graham
- Rafael Palacios
- Todd Chapman
- J. Murua
- Philippe Geuzaine
- Matthew J. Zahr
In Computational Mechanics
- Philip Avery
- Charbel Farhat
- Matthew J. Zahr
- Todd Chapman
- K. Zee
- Philippe Geuzaine
- Julia Maria Graham
- Rafael Palacios
Citations in the corpus
- A multilevel projection‐based model order reduction framework for nonlinear dynamic multiscale problems in structural and solid mechanics (2017, methodology): “The nonlinear, multiscale, PMOR framework described in the previous sections of this paper was implemented by the authors in the general-purpose FE software AERO-S [50, 51].”
- Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012, methodology): “These methods have therefore found very limited applications so far in aircraft aeroelasticity and flight dynamics with large wing deformations [19–21].”
- Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity (2006, methodology): “1 This work was done while the author was visiting the University of Colorado at Boulder.”
- The GNAT method for nonlinear model reduction: Effective implementation and application to computational fluid dynamics and turbulent flows (2012, unknown): “To assess GNAT’s performance on large-scale CFD applications, GNAT is implemented in the massively parallel compressible-flow solver AERO-F [42, 43].”
- Structure‐preserving, stability, and accuracy properties of the energy‐conserving sampling and weighting method for the hyper reduction of nonlinear finite element dynamic models (2015, methodology): “The ECSW hyper-reduction method discussed in this paper was implemented in the comprehensive FE structural analyzer AERO-S [37, 38].”