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Boundary Layer Ingesting Inlet / Distortion-Tolerant Fan (BLI2DTF) Propulsion for Highly Efficient Subsonic Cruise Aircraft.

机译：边界层摄取入口/抗扭曲风扇（BLI2DTF）推进高效亚音速巡航飞机。

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作者
Arend, D.; Hirt, S.; Sirbaugh, J.; Bakhle, M.; Wolter, J.; Cousins, W.; Tillman, G.; Voytovych, D.; Sharma, O.; Obrien, W.; Ferrar, A.;
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年度 2016
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
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1. Aeromechanical Response of a Distortion-Tolerant Boundary Layer Ingesting Fan [J] . Provenza Andrew J., Duffy Kirsten P., Bakhle Milind A. Journal of Engineering for Gas Turbines and Power . 2019,第1期

机译：变形容限边界层进气风扇的气动力学响应
2. A preliminary method to estimate impacts of inlet flow distortion on boundary layer ingesting propulsion system design point performance [J] . Chengyuan Liu, Daniel Ihiabe, Panagiotis Laskaridis, Proceedings of the Institution of Mechanical Engineers . 2014,第G9期

机译：一种估算进气流畸变对边界层进气推进系统设计点性能影响的初步方法
3. Fan Response to Boundary-Layer Ingesting Inlet Distortions [J] . Giuliani James E., Chen Jen-Ping AIAA Journal . 2016,第10期

机译：风扇对边界层进气口变形的响应
4. AEROMECHANIC RESPONSE OF A COUPLED INLET-FAN BOUNDARY LAYER INGESTING DISTORTION-TOLERANT FAN [C] . G. S. Heinlein, M. A. Bakhle, J. P. Chen ASME Turbo Expo: Turbomachinery Technical Conference and Exposition . 2019

机译：耦合进风扇边界层进气变形风扇的气动响应
5. Adjoint Design Optimization for Boundary Layer Ingesting Inlet Guide Vanes with Distorted Inlet Profiles in SU2 [D] . Baig, Aman uz zaman. 2020

机译：边界层摄取入口导向叶片的伴随设计优化，SU2中扭曲入口剖面
6. Experimental Demonstration of a Highly Efficient Fan-out Polarization Grating [O] . Chenhao Wan, Jian Chen, Xiahui Tang, -1

机译：高效扇出偏振光栅的实验演示
7. Distributed Propulsion featuring Boundary Layer Ingestion Engines for the Blended Wing Body Subsonic Transport [O] . Kok, H.J.M., Voskuijl, M., Van Tooren, M.J.L. 2010

机译：具有边界层进气引擎的分布式推进系统，用于混合机翼亚音速运输

Boundary Layer Ingesting Inlet / Distortion-Tolerant Fan (BLI2DTF) Propulsion for Highly Efficient Subsonic Cruise Aircraft.

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