Excerpt from Stresses Around Rectangular Cut-Outs in Skin-Stringer Panels Under Axial Loads-II
Skin-stringer panels, although simpler than complete shells, are highly indeterminate structures. In order to reduce the labor of analyzing such panels, simplifying assumptions and special devices may be introduced. The most important device of this nature used in references 1 and 2 is a reduction of the number of stringers, which is effected by combining a number of stringers into a sub stitute single stringer. In reference 2, this reduction was carried to the extreme of using only two substitute stringers, one for the cut stringers and one for the uncut stringers, to represent one quadrant of the panel with a cut-out. The two-stringer structure can be analyzed very rapidly but, being somewhat over-simplified, cannot give an entirely satisfactory picture. In particular, the two stringer structure does not include the region of the net section; and consequently this structure neither shows the effect of length of cut-out nor gives a solution for the maximum stringer stresses. These maximum stresses must be obtained by separate assumptions. In addition, there is no obvious relation between the shear stresses in the actual structure and the shear stresses in the substitute two-stringer structure as used in reference 2.
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Librería: Forgotten Books, London, Reino Unido
Paperback. Condición: New. Print on Demand. This book introduces a simplified three-stringer method of shear-lag analysis to calculate stress distribution around rectangular cutouts in axially loaded panels. It's derived by combining a number of stringers into single stringers, which are termed "substitute stringers". This simplification allows for rapid stress analysis of panels with a cutout while providing satisfactory accuracy. The book reviews the author's previous research on the subject and provides a more complete and accurate solution. The three-stringer method is compared with the two-stringer method to demonstrate its improved accuracy in predicting stringer stresses, with some discrepancies in shear stress predictions attributed to local deformations. The book includes mathematical details of the exact and simplified three-stringer methods and provides a numerical example solved by all methods. It also presents experimental results obtained from strain surveys around cutouts, showing good agreement between calculated and observed stringer stresses. This book is a valuable resource for engineers and researchers involved in the design and analysis of aircraft structures, particularly those involving panels with cutouts. It offers a practical and accurate method for stress analysis, contributing to the safety and efficiency of aircraft design. This book is a reproduction of an important historical work, digitally reconstructed using state-of-the-art technology to preserve the original format. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in the book. print-on-demand item. Nº de ref. del artículo: 9781527860025_0
Cantidad disponible: Más de 20 disponibles
Librería: PBShop.store US, Wood Dale, IL, Estados Unidos de America
PAP. Condición: New. New Book. Shipped from UK. Established seller since 2000. Nº de ref. del artículo: LX-9781527860025
Cantidad disponible: 15 disponibles
Librería: PBShop.store UK, Fairford, GLOS, Reino Unido
PAP. Condición: New. New Book. Shipped from UK. Established seller since 2000. Nº de ref. del artículo: LX-9781527860025
Cantidad disponible: 15 disponibles