Integrating nonlinear aerodynamic and structural analysis for a complete fighter configuration
Authors:
- 1 December 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (12) , 1150-1156
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Calculation of static elastic effects on a modern high performance fighter aircraft1986
- Combined, nonlinear aerodynamic and structural method for the aeroelastic design of a three-dimensional wing in supersonic flow1986
- Calculation of Inviscid Transonic Flow over a Complete Aircraft1986
- Simulation of wing, fuselage, and wing/fuselage flowfields using a three-dimensional Euler/Navier-Stokes algorithm1985