Author:
LI Qiushi,LYU Yongzhao,PAN Tianyu,LI Da,LU Ha'nan,GONG Yifang
Funder
National Natural Science Foundation of China
China Postdoctoral Science Foundation
Aeronautics Power Foundation of China
Subject
Mechanical Engineering,Aerospace Engineering
Reference20 articles.
1. Kim H, Liou MS. Optimal shape design of mail-slot nacelle on N3-X hybrid wing-body configuration. 31st AIAA applied aerodynamics conference; 2013 Jun 24–27; San Diego, USA. Reston: AIAA; 2013.
2. Webster RS, Sreenivas K, Hyams DG, Hilbert B, Briley WR, Whitfield DL. Demonstration of sub-system level simulations: A coupled inlet and turbofan stage. 48th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit; 2012 Jul 30-Aug 01; Atlanta, USA. Reston: AIAA; 2012.
3. Multidisciplinary optimization method for designing boundary-layer-ingesting inlets;Rodriguez;J Aircraft,2009
4. Flow simulation of supersonic inlet with bypass annular duct;Kim;J Propul Power,2011
5. O’Brien DM, Calvert ME, Butler SL. An examination of engine effects on helicopter aeromechanics. AHS specialist’s conference on aeromechanics. San Francisco, CA; 2008 Jan 23–25.
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