Thermal and oxidation response of UHTC leading edge samples exposed to simulated hypersonic flight conditions

Journal of the American Ceramic Society

Volumn 96, Issue 3, 2013, Pages 907-915

  Parthasarathy, Triplicane A ^a,b   Petry, Melvin D ^a,b   Cinibulk, Michael K ^a   Mathur, Tarun ^c   Gruber, Mark R ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UES INC   (United States)

^c ISSI   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMAL; EXPOSED TO; GLASSY LAYERS; HYPERSONIC FLIGHTS; OXIDATION MODEL; OXIDATION RESPONSE; PHYSICS-BASED MODELS; SHARP LEADING EDGES;

HEAT FLUX; HYPERSONIC AERODYNAMICS; SILICA; SILICON CARBIDE;

OXIDATION;

EID: 84875249285     PISSN: 00027820     EISSN: 15512916     Source Type: Journal    
DOI: 10.1111/jace.12180     Document Type: Article

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