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Stresses around Rectangular Cut-outs in Skin-Stringer Panels under Axial Loads. II / Paul Kuhn, John E. Duberg, Simon H. Diskin.

Knovel Aerospace Radar Technology Academic Available online

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Format:
Book
Author/Creator:
Kuhn, Paul, author.
Duberg, John E., author.
Diskin, Simon H., author.
Series:
Wartime Reports (United States. National Advisory Committee for Aeronautics) ; L-368.
NACA Wartime Report ; L-368
Language:
English
Subjects (All):
Strains and stresses.
Physical Description:
1 online resource (46 pages) : illustrations.
Other Title:
Stresses around Rectangular Cut-outs in Skin-Stringer Panels under Axial Loads - II
Place of Publication:
Washington, D.C. : National Advisory Committee for Aeronautics/NASA, 1943.
Summary:
Cut-outs in wings or fuselages produce stress concentrations that present a serious problem to the stress analyst. As a partial solution of the general problem, this paper presents formulas for calculating the stress distribution around rectangular cut-outs in axially loaded panels. The formulas are derived by means of the substitute-stringer method of shear-lag analysis.
Notes:
Description based on publisher supplied metadata and other sources.
ISBN:
1-68015-648-9

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