State of stress in and near reinforced frame subjected to concentrated loads and moments and supported in circular shell, applicable to aircraft fuselages and ballistic missile bodies, is investigated and shown to be mainly dependent upon single parameter. D-400 57 p: Basic Theory. D-401 48 p: Discontinuities of Circumferential-Bending Stiffness in Axial Direction. D-402 136 p: Applications; tables. (Work originally prepared by Lockheed Missiles and Space Div).
Analysis of frame-reinforced cylindrical shells, R.H. Macneal
NASA -- Tech Note
National Aeronautics and Space Administration -- Technical Notes ; n D-400-D-402
1960
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English
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MacNeal: Simuliertes Eintauchen
Online Contents | 1996
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