A method for analyzing the natural vibration characteristics of plate-beam combination structures is presented. Structures of built up delta wings and fuselages are used as examples. Numerical analyses of the aerodynamic characteristics in supersonic flight are developed. Vibration tests were conducted to provide a comparison with the simulation tests. (Author)
On the Natural Vibration of Plate-Beam Combination Structures, 3
1972
33 pages
Report
No indication
English
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