Aerodynamics and Propulsive Efficiency of a Blended-Wing-Body Aircraft with Distributed Propulsion System During Takeoff
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[1] P.J. Masson,et al. Next Generation More-Electric Aircraft: A Potential Application for HTS Superconductors , 2009, IEEE Transactions on Applied Superconductivity.
[2] David Rodriguez,et al. A multidisciplinary optimization method for designing boundary layer ingesting inlets , 2001 .
[3] Meng-Sing Liou,et al. Mail-Slot Nacelle Shape Design for N3-X Hybrid Wing-Body Configuration , 2015 .
[4] Hyun Dae Kim,et al. Low Noise Cruise Efficient Short Take-Off and Landing Transport Vehicle Study , 2006 .
[5] D. K. Hall,et al. Conceptual Design of an N+3 Hybrid Wing Body Subsonic Transport , 2010 .
[6] Serhat Hosder,et al. Propulsion and Aerodynamic Performance Evaluation of Jet-Wing Distributed Propulsion , 2010 .
[7] Dong-Jin Sheen,et al. Numerical simulation of Aerodynamic Characteristics of a BWB UCAV Configuration with Transition models , 2015 .
[8] R. H. Liebeck,et al. Design of the Blended Wing Body Subsonic Transport , 2002 .
[9] Bernard Grossman,et al. Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion , 2013 .