Experimental Investigations Of Surface Interactions Of Shock Heated Gases On High Temperature Materials Using High Enthalpy Shock Tubes

Experimental Investigations Of Surface Interactions Of Shock Heated Gases On High Temperature Materials Using High Enthalpy Shock Tubes

The re-entry space vehicles encounter high temperatures when they enter the earth atmosphere and the high temperature air in the shock layer around the body undergoes partial dissociation. Also, the gas molecules injected into the shock layer from the ablative thermal protection system (TPS) undergo...

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Bibliographic Details
Main Author: Jayaram, V
Other Authors: Reddy, K P J
Language:en_US
Published: 2009
Subjects:
Surface Engineering
Aerospace Materials
Shock Tubes
Shock Heated Gases
Thermal Protection System
Free Piston Driven Shock Tube
Pure Metals - Surface Nitridation
Carbon Nitride - Synthesis
Aluminium Thin Films
Aerothermochemistry
Re-entry Space Vehicles
Shock Heated Oxygen Gas
Hypersonic Shock Tunnel
Free Piston Driven Shock Tunnel (FPST)
Materials Science
Online Access:http://hdl.handle.net/2005/495

Internet

http://hdl.handle.net/2005/495

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