Thermal cracking and heat sink capacity of aviation kerosene under supercritical conditions

45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2009, Pages

  Zhong, Fengquan ^a   Fan, Xuejun ^a   Wang, Jing ^a   Yu, Gong ^a   Li, Jianguo ^a   Sung, Chih Jen ^b  

^a INSTITUTE OF MECHANICS   (China)

^b UNIVERSITY OF CONNECTICUT   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMICAL HEAT; COMPOSITION ANALYSIS; CONTROL VOLUMES; ENDOTHERMICITY; FUEL CONVERSION; FUEL TEMPERATURE; GASEOUS PRODUCTS; HEAT SINK CAPACITY; HEATING SYSTEM; LIQUID PRODUCTS; OPERATION CONDITIONS; PRESSURE RANGES; REGENERATIVE COOLING; RESIDENCE TIME; SATURATED HYDROCARBONS; SUPERCRITICAL CONDITION; TEMPERATURE RANGE; THERMAL CRACKING;

AVIATION; BENZENE; COOLING SYSTEMS; FUELS; GAS CHROMATOGRAPHY; HEAT SINKS; KEROSENE; LIQUID CHROMATOGRAPHY; LIQUIDS; METHANE; NAPHTHALENE; ORGANIC COMPOUNDS; PROPULSION;

CRACKING (CHEMICAL);

EID: 77957844115     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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