edbgtr
Aerospace
- May 3, 2001
- 101
G’Day Eng-Tippers,
A question for detail stress engineers regarding stringer beam-column compression analysis.
It has come to my notice that new forms of skin stringer construction has led to changes in stringer support conditions at the frames or ribs through which they pass. In the past, where a stringer passed through a mousehole in a frame or rib, the stringer was positively attached by fasteners to the rib or frame by means of a clip. With the loose skins no longer being attached by fasteners to the underlying airframe skeleton, but as preassembled “covers” comprising of skin and bonded-on stringers, the clips are no longer in use.
The question is this: when analysing the beam-column action of a stringer running the semi-span of, for example, a horizontal or vertical stabiliser, how are the supports at the frames or ribs considered for this analysis? In the past a correctly designed, and stabilised, clip attachment to the rib or frame could be considered a simple support for the stringer at each rib or frame station. Now, the support at the rib or frame depends on the short “overhang” beam-action of the sheet/doubler material between the stringer and the closest fastener at the edge of the mousehole in the rib or frame flange. The actual spring constant (stiffness) change from the clip support to the overhang skin support is considerable. How is this now being dealt with in analysis? Has it been determined that the overhang skin support is sufficient to still consider the stringer to be simply supported at the frame or rib?
I thank you in advance for your response.
Ed.
A question for detail stress engineers regarding stringer beam-column compression analysis.
It has come to my notice that new forms of skin stringer construction has led to changes in stringer support conditions at the frames or ribs through which they pass. In the past, where a stringer passed through a mousehole in a frame or rib, the stringer was positively attached by fasteners to the rib or frame by means of a clip. With the loose skins no longer being attached by fasteners to the underlying airframe skeleton, but as preassembled “covers” comprising of skin and bonded-on stringers, the clips are no longer in use.
The question is this: when analysing the beam-column action of a stringer running the semi-span of, for example, a horizontal or vertical stabiliser, how are the supports at the frames or ribs considered for this analysis? In the past a correctly designed, and stabilised, clip attachment to the rib or frame could be considered a simple support for the stringer at each rib or frame station. Now, the support at the rib or frame depends on the short “overhang” beam-action of the sheet/doubler material between the stringer and the closest fastener at the edge of the mousehole in the rib or frame flange. The actual spring constant (stiffness) change from the clip support to the overhang skin support is considerable. How is this now being dealt with in analysis? Has it been determined that the overhang skin support is sufficient to still consider the stringer to be simply supported at the frame or rib?
I thank you in advance for your response.
Ed.