干旱区生态环境知识资源中心(Arid): Lightweight two-stroke cycle aircraft diesel engine technology enablement program, volume 3

Arid

报告编号	NASA-CR-174923-VOL-3, NAS 1.26:174923-VOL-3
来源ID	NTRS_Document_ID: 19860003862
	Lightweight two-stroke cycle aircraft diesel engine technology enablement program, volume 3
	Freen, P. D.; Berenyi, S. G.; Brouwers, A. P.; Moynihan, M. E.
英文摘要	An experimental Single Cylinder Test Engine Program is conducted to confirm the analytically projected performance of a two-stroke cycle diesel engine for aircraft applications. Testing confirms the ability of a proposed 4-cylinder version of such an engine to reach the target power at altitude in a highly turbocharged configuration. The experimental program defines all necessary parameters to permit design of a multicylinder engine for eventual flight applications.
英文关键词	AIRCRAFT ENGINES DIESEL ENGINES FUEL INJECTION HIGH PRESSURE PISTON ENGINES SCAVENGING SUPERCHARGERS CERAMICS EXPERIMENTATION FINITE ELEMENT METHOD INTERNAL COMBUSTION ENGINES METALS
出版年	1985
报告类型	Technical Report
语种	英语
国家	美国
URL	http://hdl.handle.net/2060/19860003862
资源类型	科技报告
条目标识符	http://119.78.100.177/qdio/handle/2XILL650/259036
推荐引用方式 GB/T 7714	Freen, P. D.,Berenyi, S. G.,Brouwers, A. P.,et al. Lightweight two-stroke cycle aircraft diesel engine technology enablement program, volume 3,1985.