Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II /

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...

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Bibliographic Details

Main Author:	Kuhn, Paul
Corporate Authors:	Knovel (Firm), Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Other Authors:	Duberg, John E. (John Edward), 1917-, Diskin, Simon H.
Format:	eBook
Language:	English
Published:	Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943.
Series:	NACA WR ; L-368
Subjects:	Strains and stresses. Aerodynamics > Research. Electronic books.
Online Access:	Connect to the full text of this electronic book