Development of a test to evaluate aerothermal response of materials to hypersonic flow using a scramjet wind tunnel

International Journal of Applied Ceramic Technology

Volumn 8, Issue 4, 2011, Pages 832-847

  Parthasarathy, Triplicane A ^a,c   Petry, M Dennis ^a,c   Jefferson, George ^a   Cinibulk, Michael K ^a   Mathur, Tarun ^b   Gruber, Mark R ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b ISSI   (United States)

^c UES INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMAL; HIGH TEMPERATURE; LEADING EDGE; SAMPLE HOLDERS; SCRAMJET ENGINES; SHORT-TERM EXPOSURE; STRUCTURAL MODELS;

FREE FLIGHT; HYPERSONIC FLOW; MODEL STRUCTURES; RATING; SILICON CARBIDE; WIND TUNNELS;

HYPERSONIC AERODYNAMICS;

EID: 79960057282     PISSN: 1546542X     EISSN: 17447402     Source Type: Journal    
DOI: 10.1111/j.1744-7402.2010.02515.x     Document Type: Article

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