共 13 条
[1]
Effects of stability margin and thrust specific fuel consumption constrains on multi-disciplinary optimization for blended-wing-body design[J] Minghui ZHANG;Zhenli CHEN;Zhaoguang TAN;Wenting GU;Dong LI;Changsheng YUAN;Binqian ZHANG; Chinese Journal of Aeronautics 2019, 08
[3]
A new dynamic pushback control method for reducing fuel-burn costs: Using predicted taxi-out time[J] Guan LIAN;Yaping ZHANG;Zhiwei XING;Qian LUO;Shaowu CHENG; Chinese Journal of Aeronautics 2019, 03
[4]
Design and optimization of a novel electrically controlled high pressure fuel injection system for heavy fuel aircraft piston engine[J] Ke ZHANG;Xudong HUANG;Zhifeng XIE;Ming ZHOU; Chinese Journal of Aeronautics 2018, 09
[5]
Experimental comparison between aircraft fuel tank inerting processes using NEA and MIG[J] Lei SHAO;Weihua LIU;Chaoyue LI;Shiyu FENG;Chenchen WANG;Jun PAN; Chinese Journal of Aeronautics 2018, 07
[6]
Experimental study of an aircraft fuel tank inerting system[J] Cai Yan;Bu Xueqin;Lin Guiping;Sun Bing;Zeng Yu;Li Zixuan; Chinese Journal of Aeronautics 2015, 02
[8]
Effect of scrubbing efficiency on fuel scrubbing inerting for aircraft fuel tanks[J] Lei Shao;Shiyu Feng;Chaoyue Li;Weihua Liu;Xuying Huang Aircraft Engineering and Aerospace Technology 2019,
[9]
Experimental Comparison of Fuel Scrubbing Inerting Process Using Nitrogen and Carbon Dioxide of Aircraft Fuel Tanks[J] Shao Lei;Liu Weihua;Li Chaoyue;Feng Shiyu;Sun Bing;Pan Jun Fire Technology 2018,
[10]
Experimental Study of an On-board Fuel Tank Inerting System[J] Fei Wu;Guiping Lin;Yu Zeng;Rui Pan;Haoyang Sun IOP Conference Series: Materials Science and Engineering 2017,