Isbn: 9781527860025 - stresses around rectangular cut-outs in skin-stringer panels under axial loads-ii (classic reprint) (3 risultati)

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Da: PBShop.store US, Wood Dale, IL, U.S.A.PBShop.store US
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 26,20
Spedizione gratuitaSpedito in U.S.A.Quantità: 15 disponibili
PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

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Da: PBShop.store UK, Fairford, GLOS, Regno UnitoPBShop.store UK
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 25,32
EUR 3,83 spedizioneSpedito da Regno Unito a U.S.A.Quantità: 15 disponibili
PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

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- Print on Demand
Da: Forgotten Books, London, Regno UnitoForgotten Books
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EUR 16,72
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Paperback. Condizione: 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.…