Active Flutter Suppression - An Emerging Technology
暂无分享,去创建一个
[1] J. I. Arnold,et al. Flight test evaluation of an advanced stability augmentation system for B-52 aircraft. , 1969 .
[2] R. M. Bennett,et al. A Wind-Tunnel Technique for Measuring Frequency-Response Functions for Gust Load Analyses , 1965 .
[3] K. L. Roger,et al. Evaluation of B-52 structural response to random turbulence with stability augmentation systems. , 1967 .
[4] E. L. S. Lum,et al. Linear Optimal Theory Applied to Active Structural Bending Control , 1968 .
[5] L. Edinger. Design of elastic mode suppression systems for ride quality improvement and application to an SST , 1967 .
[6] J. Polve. The state of ignorance of flutter-flight testing , 1966 .
[7] R. Swaim,et al. Controlling dynamic response in rough air , 1966 .
[8] J. H. Wykes,et al. Structural dynamic stability augmentation and gust alleviation of flexible aircraft. , 1968 .
[9] W. J. Rohling. Flying qualities - An integral part of a stability augmentation system , 1969 .