Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration (English)
- New search for: Zhang, Jing
- New search for: Kang, Wenwen
- New search for: Yang, Lingyu
- New search for: Zhang, Jing
- New search for: Kang, Wenwen
- New search for: Yang, Lingyu
In:
Aircraft Engineering and Aerospace Technology
;
91
, 10
;
1285-1294
;
2019
-
ISSN:
- Article (Journal) / Electronic Resource
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Title:Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration
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Contributors:
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Published in:Aircraft Engineering and Aerospace Technology ; 91, 10 ; 1285-1294
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Publisher:
- New search for: Emerald Publishing Limited
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Publication date:2019-08-19
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Size:1 pages
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ISSN:
-
DOI:
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Type of media:Article (Journal)
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Type of material:Electronic Resource
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Language:English
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Keywords:
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Source:
Table of contents – Volume 91, Issue 10
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1257
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A covariance shaping filtering method for tightly-coupled MIMU/GNSS of UAVLiu, Bin / Xu, Jiangtao / Fu, Bangsheng / Hao, Yong / An, Tianyu et al. | 2019
- 1268
-
Observer-based reaction wheel fault reconstruction for spacecraft attitude control systemsJia, Qingxian / Li, Huayi / Chen, Xueqin / Zhang, Yingchun et al. | 2019
- 1278
-
Knock combustion investigation on a two-stroke spark ignition UAV engine burning RP-3 kerosene fuelLiu, Rui / Sheng, Jing / Ma, Jie / Yang, Guang / Dong, Xuefei / Liang, Yongsheng et al. | 2019
- 1285
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Aerodynamic benefits of boundary layer ingestion for distributed propulsion configurationZhang, Jing / Kang, Wenwen / Yang, Lingyu et al. | 2019
- 1295
-
Impact of mission requirements on the design of low observable UCAV configurationsSepulveda Palacios, Eduardo / Smith, Howard et al. | 2019
- 1308
-
Simultaneous tailplane of small UAV and autopilot system designÇoban, Sezer et al. | 2019
- 1314
-
Derivation of knockdown factors for grid-stiffened cylinders considering various shell thickness ratiosSim, Chang-Hoon / Kim, Han-Il / Park, Jae-Sang / Lee, Keejoo et al. | 2019
- 1327
-
Influence of milling toolpaths in machining of the turbine bladeJarolmasjed, Seyedamin / Davoodi, Behnam / Pourebrahim Alamdari, Babak et al. | 2019
- 1340
-
Supersonic jet flow control using semi-circular corrugated tabsK., Sathish Kumar / Chidambaram, Senthilkumar et al. | 2019