Thermal Shock Resistance of Ultra-High-Temperature Ceramics Under Aerodynamic Thermal Environments-Reference-Cited by-同舟云学术

Thermal Shock Resistance of Ultra-High-Temperature Ceramics Under Aerodynamic Thermal Environments

Published:2013-04 Issue:4 Volume:51 Page:840-848
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Cheng Tianbao¹,Li Weiguo²,Fang Daining³

Affiliation:

1. Department of Engineering Mechanics, Chongqing University, 400030 Chongqing, People’s Republic of China

2. Department of Engineering Mechanics, State Key Laboratory of Coal Mine Disaster Dynamics and Control, Chongqing University, 400030 Chongqing, People’s Republic of China

3. College of Engineering, State Key Laboratory for Turbulence and Complex Systems, Peking University, 100871 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051750

Reference30 articles.

1. Refractory Diborides of Zirconium and Hafnium

2. Thermal Conductivity Characterization of Hafnium Diboride-Based Ultra-High-Temperature Ceramics

3. EFFECTS OF THERMAL ENVIRONMENTS ON THE THERMAL SHOCK RESISTANCE OF ULTRA-HIGH TEMPERATURE CERAMICS

4. KaufmanL. “Boride Composites—A New Generation of Nose Cap and Leading Edge Materials for Reuseable Lifting Re-entry Systems,” AIAA Paper 70-0278, Feb. 1970.

5. Mechanical, Thermal, and Oxidation Properties of Refractory Hafnium and zirconium Compounds

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