论文信息 - Flutter boundary for simply supported unstiffened cylinders. - 字舞流文

Flutter boundary for simply supported unstiffened cylinders.

Semiempirical stability boundary for flutter of simply supported cylinders for various length- radius and radius-thickness ratios

S. C. Dixon | M. L. Hudson

[1] S. C. Dixon,et al. Flutter, vibration, and buckling of truncated orthotropic conical shells with generalized elastic edge restraint, supplement , 1970 .

[2] L. L. Carter,et al. SOME ASPECTS OF CYLINDRICAL SHELL PANEL FLUTTER. , 1967 .

[3] H. Voss,et al. The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical Shells , 1961 .

[4] L. C. Woods. The theory of subsonic plane flow , 1961 .

[5] J. Hedgepeth,et al. Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds , 1957 .

[6] Y. C. Fung,et al. SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCH , 1963 .

[7] Y. C. Fung,et al. Comparing theory and experiment for the supersonic flutter of circular cylindrical shells. , 1967 .