Author:
Valencia Esteban,Hidalgo Victor
Reference29 articles.
1. Felder J, Kim H, Brown G. Turboelectric distributed propulsion engine cycle analysis for hybrid-wing-body aircraft. In: 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition; 2009. p. 1132
2. Plas A. Performance of a boundary layer ingesting propulsion system [MSc. thesis], Massachusetts Institute of Technology, [MSc. thesis], Dept. of Aeronautics and Astronautics, Massachusetts, USA, 2006
3. Valencia EA, Nalianda D, Laskaridis P, Singh R. Methodology to assess the performance of an aircraft concept with distributed propulsion and boundary layer ingestion using a parametric approach. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2015;229(4):682-693
4. Gundlach J. Designing Unmanned Aircraft Systems: A Comprehensive Approach. American Institute of Aeronautics and Astronautics, Inc.1801 Alexander Bell Drive, Reston, Virginia, 2012, 20191-4344
5. Valencia E, Hidalgo V, Cisneros J. Design point analysis of a distributed propulsion system with boundary layer ingestion implemented in UAV’s for agriculture in the Andean region. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference, Salt Lake City, Utah, 2016
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献