Integrating nonlinear aerodynamic and structural analysis for a complete fighter configuration
Author:
Affiliation:
1. Planning Research Corporation, Hampton, Virginia
2. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45715
Reference13 articles.
1. 2"Static Aeroelasticity in Combat Aircraft,"AGARD Rep. 725, Jan. 1986.
2. Combined, nonlinear aerodynamic and structural method for the aeroelastic design of a three-dimensional wing in supersonic flow
3. Calculation of static elastic effects on a modern high performance fighter aircraft
4. Calculation of Inviscid Transonic Flow over a Complete Aircraft
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