Skin, Stringer, and Fastener Loads in Buckled Fuselage Panels¶
Young, R. D., Rose, C. A., & Starnes Jr, J. H. (2001). Skin, Stringer, and Fastener Loads in Buckled Fuselage Panels.
Cited by¶
1 citation across 1 artifact.
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Domain-specific¶
- Stressed Skin
- An original fuselage-panel study models such redistribution under particular buckling and pressure conditions; it illustrates the need to inspect the case rather than supplying a universal stress rule.
This sourceOriginal research abstract inspected for modeled load redistribution in a buckled fuselage panel; it does not prove a general stress allocation.
- An original fuselage-panel study models such redistribution under particular buckling and pressure conditions; it illustrates the need to inspect the case rather than supplying a universal stress rule.
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Registry ID ref:98a197b3c937 · see in the full table