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- W766161735 abstract "The buckling characteristics of a hypersonic beaded skin panel were investigated under pure compression with boundary conditions similar to those found in a wing mounted condition. The primary phases of analysis reported include: (1) experimental testing of the panel to failure; (2) finite element structural analysis of the beaded panel with the computer program NASTRAN; and (3) summary of the semiclassical buckling equations for the beaded panel under purely compressive loads. A comparison of each of the analysis methods is also included." @default.
- W766161735 created "2016-06-24" @default.
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- W766161735 date "1977-12-01" @default.
- W766161735 modified "2023-09-27" @default.
- W766161735 title "Structural analysis of ultra-high speed aircraft structural components" @default.
- W766161735 hasPublicationYear "1977" @default.
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