Integrating nonlinear aerodynamic and structural analysis for a complete fighter configuration
- 1 December 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (12) , 1150-1156
- https://doi.org/10.2514/3.45715
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Calculation of static elastic effects on a modern high performance fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Combined, nonlinear aerodynamic and structural method for the aeroelastic design of a three-dimensional wing in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Calculation of Inviscid Transonic Flow over a Complete AircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Simulation of wing, fuselage, and wing/fuselage flowfields using a three-dimensional Euler/Navier-Stokes algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985