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Experimental Characterization of Nonlinear Damping in the F-16 Wing Structure
Journal of Aircraft ( IF 1.5 ) Pub Date : 2020-08-13 , DOI: 10.2514/1.c035850 Charles M. Denegri 1 , Vinod K. Sharma 2 , Lynn J. Neergaard 2
Journal of Aircraft ( IF 1.5 ) Pub Date : 2020-08-13 , DOI: 10.2514/1.c035850 Charles M. Denegri 1 , Vinod K. Sharma 2 , Lynn J. Neergaard 2
Affiliation
Earlier work did not find any static stiffness nonlinearities in the F-16 wing structure, but suggested that dynamic nonlinearities may be present. Computational studies have demonstrated that smal...
中文翻译:
F-16 机翼结构非线性阻尼的实验表征
早期的工作没有在 F-16 机翼结构中发现任何静态刚度非线性,但表明可能存在动态非线性。计算研究表明,小...
更新日期:2020-08-13
中文翻译:
F-16 机翼结构非线性阻尼的实验表征
早期的工作没有在 F-16 机翼结构中发现任何静态刚度非线性,但表明可能存在动态非线性。计算研究表明,小...