Numerical Study on Structure Thermal Protection of Aerospace Plane

Abstract:

The letter relying on the status of existing thermal protection system and existing flight parameters, appropriate metal thermal protection system being able to reproduced are designed; according to the distribution of heat-flow density we make certain the structure and thickness of the heat shield, structure of cooling bed and pressure of cooling air, velocity of flow and so on. The distributions of temperature of points on the nose and the inside of skin are calculated.

• Periodical: Advanced Materials Research (Volume 900)
• Pages: 814-817
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.900.814
• Online since: February 2014
• Authors: Shuang Chen, Qing Feng Zhang
• Keywords: Aerodynamic Heating, Aerospace, Metal Thermal Protection, Reproduced

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