4. Advanced Materials and Structures for High Temperature Applications

Papers

1. Emissivity Analyses Of Materials Candidate For Eart’s Atmosphere Re-Entry From Space Missions

2. estimation of surface heat flux for ablation and charring of thermal protection material

3. Plasma Wind Tunnel Tests for C/SiC Composite with Additional Mechanical Tensile Load

4. Dynamic response testing and analysis of hypersonic aircraft panels excited by high-intensity acoustic loads in thermal environment

5. A new type scramjet thermal protection structure based on high temperature heat pipe technique

7. design study on multi-layered stand-off thermal protection system using porous titanium sandwich panels

8. A New Reusable Thermal Protection System Concept for Earth Atmospheric Re-Entry

9. Hybrid Ablative/Ceramic Thermal Protection System: Mission Profile, Materials Selection, Interface Development and Verification Approach

10. A Comparative Assessment of Criticality of Local Damage in Composite Liner of a Nozzle Through Finite Element Thermal-Structural Analysis

11. Thermally and Dimensionally Stable Structures of Carbon-Carbon Laminated Composites for Space Applications

12. The Ablative Performance of Light Weight Charring Ablators in High Enthalpy Environment

13. Heat Pipe Cooled Leading Edges