A Hybrid State Vector Approach to Aeroelastic Analysis
- 1 October 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (10) , 1442-1449
- https://doi.org/10.2514/3.51205
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Asymptotic Integration Methods Applied to Rotating BeamsJournal of Applied Mechanics, 1980
- Asymptotic Solutions Without Special Functions for Steep and Shallow ShellsPublished by Elsevier ,1980
- Forward Swept Wing Static AeroelasticityPublished by Defense Technical Information Center (DTIC) ,1979
- An aeroelastic optimization procedure for composite high aspect ratio wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Applications of Laplace transform methods to airfoil motion and stability calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- Unsteady aerodynamic modeling for arbitrary motionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Matrix Eigensystem Routines — EISPACK GuidePublished by Springer Nature ,1974
- On a Variational Theorem in ElasticityJournal of Mathematics and Physics, 1950
- The Flutter of a Uniform Cantilever WingJournal of Applied Mechanics, 1945