Nonlinear Flight Dynamics of Very Flexible Aircraft
- 1 September 2007
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 44 (5), 1528-1545
- https://doi.org/10.2514/1.27606
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
- Flight Loads Analysis with Inertially Coupled Equations of MotionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Comparison of Unsteady Aerodynamic Modelling Methodologies with Respect to Flight Loads AnalysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Future of Airplane AeroelasticityJournal of Aircraft, 2003
- Aeroelasticity of Nonconventional Airplane Configurations-Past and FutureJournal of Aircraft, 2003
- Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance AircraftJournal of Aircraft, 2001
- Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic FlowJournal of Aircraft, 2000
- Renaissance of Aeroelasticity and Its FutureJournal of Aircraft, 1999
- Modeling and simulation of flexible flight vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Response of B-2 aircraft to nonuniform spanwise turbulenceJournal of Aircraft, 1993
- Aeroelastic characteristics of a highly flexible aircraftJournal of Aircraft, 1990