A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads

Y. Xiong,

doi:10.1515/SECM.1999.8.5.243

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A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads

Y. Xiong,

Published/Copyright: October 1, 1999

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From the journal Science and Engineering of Composite Materials Volume 8 Issue 5

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Xiong,, Y.. "A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads" Science and Engineering of Composite Materials, vol. 8, no. 5, pp. 243-256. https://doi.org/10.1515/SECM.1999.8.5.243

Xiong,, Y. (). A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads. Science and Engineering of Composite Materials, 8(5), 243-256. https://doi.org/10.1515/SECM.1999.8.5.243

Xiong,, Y. () A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads. Science and Engineering of Composite Materials, Vol. 8 (Issue 5), pp. 243-256. https://doi.org/10.1515/SECM.1999.8.5.243

Xiong,, Y.. "A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads" Science and Engineering of Composite Materials 8, no. 5 (): 243-256. https://doi.org/10.1515/SECM.1999.8.5.243

Xiong, Y. A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads. Science and Engineering of Composite Materials. ;8(5): 243-256. https://doi.org/10.1515/SECM.1999.8.5.243

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Published Online: 1999-10

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TABLE OF CONTENTS
Residual Strength Degradation of a Titanium Matrix Composite Subjected to Elevated Temperature Fatigue
A Complex Variational Approach for Single Loaded/Unloaded Hole in Finite Laminated Plate Under General In-Plane Loads
High Temperature Interactions of Metal Oxides and Carbides with Ionic Salts
An Overview of Intermetallic Matrix Composites Based on Ti3Al and TiAl

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