[PDF.09ah] Boundary Element Methods for Damage Tolerance Design of Aircraft Structures (Topics in Engineering, Volume 33)

Boundary Element Methods for Damage Tolerance Design of Aircraft Structures (Topics in Engineering, Volume 33)

[PDF.yn36] Boundary Element Methods for Damage Tolerance Design of Aircraft Structures (Topics in Engineering, Volume 33)

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 | #10263112 in Books |  1998-04-21 | Original language:English | PDF # 1 |  10.00 x6.75 x.75l, | File type: PDF | 192 pages

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|| |The book is very useful in promoting further research leading to integrated systems of analysis and design of stiffened panels. It can also be used as an auxiliary text for courses on fracture mechanics or applications of boundary integral methods. --Applied M

This book presents dual boundary element formulations for two-dimensional analysis of the damage tolerance of patch-repaired stiffened panels and sheets used in aircraft. The discussion demonstrates the reliability of the formulation and covers adhesively bonded, integral and mechanically fastened stiffeners, riveted and bonded repairs consisting of single or double patches, and elastic and elastic-plastic attachment models. The author presents some new formulations to e...

You easily download any file type for your device.Boundary Element Methods for Damage Tolerance Design of Aircraft Structures (Topics in Engineering, Volume 33)   |  Nelson Salgado. I was recommended this book by a dear friend of mine.

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