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Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications

National Aeronautics and Space Administration
4.9/5 (20582 ratings)
Description:Titanium matrix composites (TMCs) have been extensively evaluated for their potential to replace conventional superalloys in high temperature structural applications, with significant weight-savings while maintaining comparable mechanical properties. New gamma titanium aluminide alloys and an appropriate fiber could offer an improved TMC for use in intermediate temperature applications (400-800 C). The purpose of this investigation is the evaluation of a gamma titanium aluminide alloy with nominal composition Ti-46.5Al-4(Cr, Nb, Ta, B)at.% as a structural material in future aerospace transportation systems, where very light-weight structures are necessary to meet the goals of advanced aerospace programs.Johnson, W. Steven and Weeks, Carrell E.Langley Research CenterMECHANICAL PROPERTIES; STRUCTURAL DESIGN; TITANIUM ALUMINIDES; HYPERSONIC FLIGHT; HEAT RESISTANT ALLOYS; X-43 VEHICLE; TEMPERATURE; FEASIBILITY ANALYSIS; THERMAL PROTECTION; METAL MATRIX COMPOSITES; FAILURE MODES; YIELD STRENWe have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications. To get started finding Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
100
Format
PDF, EPUB & Kindle Edition
Publisher
Createspace Independent Publishing Platform
Release
2018
ISBN
1720511845

Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications

National Aeronautics and Space Administration
4.4/5 (1290744 ratings)
Description: Titanium matrix composites (TMCs) have been extensively evaluated for their potential to replace conventional superalloys in high temperature structural applications, with significant weight-savings while maintaining comparable mechanical properties. New gamma titanium aluminide alloys and an appropriate fiber could offer an improved TMC for use in intermediate temperature applications (400-800 C). The purpose of this investigation is the evaluation of a gamma titanium aluminide alloy with nominal composition Ti-46.5Al-4(Cr, Nb, Ta, B)at.% as a structural material in future aerospace transportation systems, where very light-weight structures are necessary to meet the goals of advanced aerospace programs.Johnson, W. Steven and Weeks, Carrell E.Langley Research CenterMECHANICAL PROPERTIES; STRUCTURAL DESIGN; TITANIUM ALUMINIDES; HYPERSONIC FLIGHT; HEAT RESISTANT ALLOYS; X-43 VEHICLE; TEMPERATURE; FEASIBILITY ANALYSIS; THERMAL PROTECTION; METAL MATRIX COMPOSITES; FAILURE MODES; YIELD STRENWe have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications. To get started finding Evaluation of a Gamma Titanium Aluminide for Hypersonic Structural Applications, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
100
Format
PDF, EPUB & Kindle Edition
Publisher
Createspace Independent Publishing Platform
Release
2018
ISBN
1720511845
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