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Volumn 24, Issue 2, 2010, Pages 609-618

Design optimization of a loop heat pipe to cool a lithium ion battery onboard a military aircraft

Author keywords

Airborne high energy laser system; Lithium ion battery; Loop heat pipe; Reliability based design optimization

Indexed keywords

AIR COOLING; ANALYTICAL SOLUTIONS; APPROXIMATION MODEL; BATTERY TEMPERATURE; BLEED AIR; DESIGN OBJECTIVES; DESIGN OPTIMIZATION; FLYING AIRCRAFT; HEAT LOADS; HIGH ENERGY; HIGH-ENERGY LASER SYSTEMS; LITHIUM-ION BATTERY; LOOP HEAT PIPE; LOOP HEAT PIPES; OPERATING TEMPERATURE; OPERATIONAL RELIABILITY; OPTIMIZATION PROCEDURES; OPTIMIZATION PROCESS; POROUS WICKS; POWER CONSUMPTION; RELIABILITY-BASED DESIGN OPTIMIZATION; THERMAL CHARACTERISTICS; THERMO-HYDRAULIC MODEL; THIN LIQUID FILM;

EID: 77949601504     PISSN: 1738494X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s12206-009-1214-6     Document Type: Article
Times cited : (57)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.