Oxidation resistant carbon-carbon composites : the effect of temperature dependent matrix material properties on laminate response /
a research area of increasing importance. As the use of the
| Main Author: | |
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| Format: | Thesis eBook |
| Language: | English |
| Published: |
[Place of publication not identified] :
[publisher not identified] ;
1994.
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| Subjects: | |
| Online Access: | Link to OAKTrust copy |
| Summary: | a research area of increasing importance. As the use of the applications, it is of critical importance to understand the are then used as model input in two dimensional axial performance of the model. The material transformation, carbon-carbon laminate. Two different through-the-thickness conjunction with internal particulate oxidation inhibitors. environments in excess of 450 OC. A common protection scheme however, is shown to affect the transverse model response. includes the use of external oxidation barrier coatings in indicate that the assumed material transformation of the influence of the oxidation of the inhibitor particles on the initial phase, the oxidation of the inhibitor particles and investigation encompasses two development phases. In the its effect on the temperature dependent material properties laminate mechanics specific to carbon-carbon composite laminates. Specifically, the materials of interest in this materials expands towards more demanding aerospace matrix material has little effect on the longitudinal or mechanical properties of the matrix material, as well as the models are subjected to a variety of longitudinal and of the inhibited matrix material are analyzed. The representations are considered. The through-the-thickness representations of the through the-thickness region of a research are oxidation resistant carbon-carbon composites. temperature dependent matrix material properties developed the catastrophic oxidation of the structure in oxygen rich The goal of this research is to gain an understanding of the The structural analysis of carbon-carbon (C-C) composites is thermomechanical performance of the laminate. This These material systems include a protection scheme to prevent transverse mechanical and thermomechanical loads. Results |
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| Item Description: | "Major subject: Mechanical Engineering". Vita. |
| Physical Description: | xi, 91 leaves : illustrations ; 28 cm. Also available online. |
| Bibliography: | Includes bibliographical references. |