Structural response of oxidation resistant carbon-carbon composites /

coated carbon-carbon laminate.

Bibliographic Details
Main Author: Ashley, Timothy Harold, 1970-
Format: Thesis eBook
Language:English
Published: [Place of publication not identified] : [publisher not identified] ; 1996.
Subjects:
Online Access:Link to OAKTrust copy

MARC

Tag First Indicator Second Indicator Subfields
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008 970630s1996 xx a b 000 0 eng d
035 |9 AHJ6649AM 
035 |a (OCoLC)37215797 
040 |a TXA  |c TXA  |d UtOrBLW 
049 |a TXAM  |a TXAR 
099 |a 1996  |a Thesis  |a A845 
100 1 |a Ashley, Timothy Harold,  |d 1970- 
245 1 0 |a Structural response of oxidation resistant carbon-carbon composites /  |c by Timothy Harold Ashley. 
264 1 |a [Place of publication not identified] :  |b [publisher not identified] ;  |c 1996. 
300 |a xi, 115 leaves :  |b illustrations ;  |c 28 cm. 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
500 |a "Major subject: Mechanical Engineering". 
500 |a Vita. 
502 |b M.S.  |c Texas A&M University  |d 1996. 
504 |a Includes bibliographical references: pages 94-95. 
520 |a coated carbon-carbon laminate. 
520 |a coatings do not provide complete protection against  
520 |a compared to test data to verify the predictions of the lamina  
520 |a composites will oxidize without a protective coating to seal  
520 |a conjunction with the coatings in order to enhance the  
520 |a defects, and oxidation on this material system subjected to  
520 |a determine the constitutive response of the carbon-carbon  
520 |a environments at temperatures above 500'C, carbon-carbon  
520 |a high temperatures, they are attractive candidates for high  
520 |a highly inhibited, eight harness satin weave, RT42 CVD SiC  
520 |a homogenization techniques, and unit cell methodology to  
520 |a laminate with the inhibitors. These analytical models are  
520 |a measured. Herein, analytical models are developed using  
520 |a oxidation resistance. The effectiveness of these  
520 |a oxidation. Secondary protection agents such as boron carbide  
520 |a particulates are added to the substrate and used in  
520 |a particulates has not yet been qualitative and quantitatively  
520 |a response. The material system studied is HITCO 2D CC137EH,  
520 |a Since carbon-carbon composites maintain their strength at  
520 |a temperature applications. Although, in oxygen rich  
520 |a the laminate from oxygen penetration. The outer protective  
520 |a thermo-mechanical loading. The analytical models are  
520 |a used to study the effects of progressive failure, material  
530 |a Also available online. 
530 |a Issued also on microfiche from Lange Micrographics. 
650 4 |a Major mechanical engineering. 
856 4 1 |u https://hdl.handle.net/1969.1/ETD-TAMU-1996-THESIS-A845  |z Link to OAKTrust copy  |t 0 
999 |a MARS 
999 f f |s 5aa51794-7b91-317c-9e4b-9fe93be5410b  |i 12a4ec25-3f6f-3eec-bf40-263698300321  |t 0 
952 f f |p noncirc  |a Texas A&M University  |b College Station  |c Cushing Memorial Library & Archives  |s cush tdrm  |d Cushing: Theses & Dissertations Microforms (Does not check out)  |t 0  |e 1996 Thesis A845  |h Other scheme  |i computer -- online resource 
952 f f |a Texas A&M University  |b College Station  |c Electronic Resources  |s www_evans  |d Available Online  |t 0  |e 1996 Thesis A845  |h Other scheme 
998 f f |a 1996 Thesis A845  |t 0  |l Cushing: Theses & Dissertations Microforms (Does not check out) 
998 f f |a 1996 Thesis A845  |t 0  |l Available Online