| タイトル | Minimum-mass design of filamentary composite panels under combined loads: Design procedure based on simplified buckling equations |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770003609 |
| 著者（英） | Agranoff, N.; Stroud, W. J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1976-10-01 |
| 言語 | eng |
| 内容記述 | An analytical procedure is presented for designing hat stiffened and corrugated panels made of composite material and subjected to longitudinal (in the direction of the stiffeners) compression and shear loadings. The procedure is based on nonlinear mathematical programming techniques and a simplified set of buckling equations. Design requirements considered are buckling, strength, and extensional and shear stiffness. The effects of specified thickness, variation of cross-section dimensions, stiffness requirements, local buckling boundary conditions, and the effect of combined compression and shear loadings are shown. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 77N10552
NASA-TN-D-8257
L-10770 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/184169 |
