Comparison of candidate architectures for future distributed propulsion electric aircraft. C Jones, P Norman, S Galloway, M Armstrong, A Bollman IEEE Transactions on Applied Superconductivity 26 (6), 2016 | 98 | 2016 |
Architecture, voltage, and components for a turboelectric distributed propulsion electric grid MJ Armstrong, M Blackwelder, A Bollman, C Ross, A Campbell, C Jones, ... | 79 | 2015 |
Revolutionary Aeropropulsion Concept for Sustainable Aviation: Turboelectric Distributed Propulsion HD Kim, JL Felder, MT Tong, M Armstrong 21st ISABE Conference, 2013 | 67 | 2013 |
Trade studies for NASA N3-X turboelectric distributed propulsion system electrical power system architecture MJ Armstrong, CAH Ross, MJ Blackwelder, K Rajashekara SAE International Journal of Aerospace 5 (2012-01-2163), 325-336, 2012 | 58 | 2012 |
Propulsion system component considerations for NASA N3-X turboelectric distributed propulsion system MJ Armstrong, CAH Ross, MJ Blackwelder, K Rajashekara SAE International Journal of Aerospace 5 (2012-01-2165), 344-353, 2012 | 53 | 2012 |
Stability, transient response, control, and safety of a high-power electric grid for turboelectric propulsion of aircraft M Armstrong, C Ross, D Phillips, M Blackwelder | 45 | 2013 |
Development and application of GT-HEAT for the electrically variable engine (TM) design D Trawick, C Perullo, M Armstrong, D Snyder, JC Tai, DN Mavris 55th AIAA Aerospace Sciences Meeting, 1922, 2017 | 34 | 2017 |
Turbo-electric distributed aircraft propulsion: Microgrid architecture and evaluation for ECO-150 DC Loder, A Bollman, MJ Armstrong 2018 IEEE Transportation Electrification Conference and Expo (ITEC), 550-557, 2018 | 27 | 2018 |
Cycle selection and sizing of a single-aisle transport with the electrically variable engine (TM)(EVE) for fleet level fuel optimization C Perullo, D Trawick, M Armstrong, JC Tai, DN Mavris 55th AIAA Aerospace Sciences Meeting, 1923, 2017 | 27 | 2017 |
Fundamentals of Parallel Hybrid Turbofan Mission Analysis with Application to the Electrically Variable Engine JC Gladin, D Trawick, D Mavris, M Armstrong, D Bevis, K Klein 2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS), 1-16, 2018 | 21 | 2018 |
Turboelectric distributed propulsion protection system design trades C Ross, M Armstrong, M Blackwelder, C Jones, P Norman, S Fletcher SAE ASTC, 2014 | 20 | 2014 |
Methodology for aircraft system architecture definition D Mavris, C de Tenorio, M Armstrong 46th AIAA aerospace sciences meeting and exhibit, 149, 2008 | 19 | 2008 |
A process for function based architecture definition and modeling MJ Armstrong | 15 | 2008 |
Function based architecture design space definition and exploration M Armstrong, C De Tenorio, D Mavris, E Garcia The 26th Congress of ICAS and 8th AIAA ATIO, 8928, 2008 | 13 | 2008 |
Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft MJ Armstrong Georgia Institute of Technology, 2011 | 12 | 2011 |
Implications of distribution voltage configuration on TeDP electrical systems M J. Armstrong, C AH Ross Aircraft Engineering and Aerospace Technology: An International Journal 86 …, 2014 | 11 | 2014 |
Sensitivity of TeDP Microgrid Systems Weight and Efficiency to Operating Voltage M Armstrong, M Blackwelder, C Ross 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014 | 10 | 2014 |
Architecture Subsystem Sizing and Coordinated Optimization Methods C de Tenorio, M Armstrong, D Mavris 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and …, 2009 | 9 | 2009 |
A pre-design sensitivity analysis tool for consideration of full-electric aircraft propulsion electrical power system architectures CE Jones, PJ Norman, SJ Galloway, GM Burt, M Armstrong, A Bollman 2015 International Conference on Electrical Systems for Aircraft, Railway …, 2015 | 8 | 2015 |
Pulse shape and duration in frontal crashes CY Warner, MH Warner, C Crosby, M Armstrong Crash Reconstruction Research 1, 239, 2008 | 8 | 2008 |