Aeroelastic Loads Predictions using Finite Element Aerodynamics
Author:
Affiliation:
1. Douglas Aircraft Company, Long Beach, Cal.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59890
Reference12 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Investigation of dynamic structural models suitable for the simulation of large aircraft;Modeling and Simulation Technologies Conference and Exhibit;1999-08-09
2. Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics;Journal of Aircraft;1985-09
3. Equations of motion of an elastic flight vehicle utilizing static aeroelastic characteristics of the restrained vehicle;25th Structures, Structural Dynamics and Materials Conference;1984-05-14
4. On the strong singular method for the problems of subsonic flow past obstacles;Applied Mathematics and Mechanics;1983-10
5. Structural design loads for future airplanes;21st Structures, Structural Dynamics, and Materials Conference;1980-05-12
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