A Superposition Method for Calculating the Aeroelastic Behavior of Swept Wings
Author:
Affiliation:
1. Boeing Airplane Company and University of Washington,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2031
Reference6 articles.
1. Some Aeroelastic Properties of Swept Wings
2. A Formulation of the Aeroelastic Problem for a Swept Wing
Cited by 7 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. Statische aeroelastische Probleme;Grundlagen der Aeroelastik;1974
2. Aeroelastic Solution for a Wing Plan Form with a Tip Control Surface;Journal of the Aerospace Sciences;1958-11
3. Equations for the Loading, Section Pitching-Moment Coefficient, and Center-of-Pressure Distributions on Triangular Wings Having Supersonic Leading and Trailing Edges for Various Basic;Journal of the Aeronautical Sciences;1956-02
4. Spanwise Variation in the Pitching-Moment Coefficient and the Center of Pressure Due to Various Basic Twist Distributions on Triangular Wings Having Supersonic Leading and Trailing Edge;Journal of the Aeronautical Sciences;1955-09
5. Estimation of the Effects of Distortion on the Longitudinal Stability of Swept Wing Aircraft at High Speeds (Sub-Critical Mach Numbers);Aeronautical Quarterly;1954-11
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