热科学学报（英文版）2011，Vol.20Issue(6)：556-562,7.DOI:10.1007/s11630-011-0510-5
The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel
The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel
Zhang Rongchun 1Fan Weijun1
作者信息
- 1. National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
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摘要
关键词
high temperature rise/evaporator/wind tunnel/combustor/aviation keroseneKey words
high temperature rise/evaporator/wind tunnel/combustor/aviation kerosene引用本文复制引用
Zhang Rongchun,Fan Weijun..The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel[J].热科学学报（英文版）,2011,20(6):556-562,7.
