Michael James Armstrong
Michael James Armstrong
Aerspace Systems Engineering Specialist, Rolls-Royce
Verified email at
Cited by
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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
Architecture, voltage and components for a turboelectric distributed propulsion electric grid
MJ Armstrong, M Blackwelder, A Bollman, C Ross, A Campbell, C Jones, ...
Revolutionary Aeropropulsion Concept for Sustainable Aviation: Turboelectric Distributed Propulsion
HD Kim, JL Felder, MT Tong, M Armstrong
21st ISABE Conference, 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
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
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
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
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
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
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
Turboelectric distributed propulsion protection system design trades
C Ross, M Armstrong, M Blackwelder, C Jones, P Norman, S Fletcher
SAE ASTC, 2014
Methodology for aircraft system architecture definition
D Mavris, C de Tenorio, M Armstrong
46th AIAA aerospace sciences meeting and exhibit, 149, 2008
A process for function based architecture definition and modeling
MJ Armstrong
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
Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft
MJ Armstrong
Georgia Institute of Technology, 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
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
Next-generation aviation li-ion battery technologies—enabling electrified aircraft
TP Barrera, JR Bond, M Bradley, R Gitzendanner, EC Darcy, M Armstrong, ...
The Electrochemical Society Interface 31 (3), 69, 2022
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
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
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