Further generalization of an equivalent plate representation for aircraft structural analysis
- 1 January 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (1) , 67-74
- https://doi.org/10.2514/3.45724
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
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- 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
- Equivalent plate analysis of aircraft wing box structures with general planform geometryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Aeroelastic tailoring studies in fighter aircraft designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979