H. Standard, Generalized Method of Propeller Performance Estimation, 1963.

P. Marconi and C. Serghine, Alternative Method for Re-starting a Helicopter Turboshaft Engine on Standby, and Multiengine Helicopter Propulsion System Allowing such a Method to be Performed, TURBOMECA Patent WO, issue.3, 2015.

B. Roth, R. Giffin, A. Th, and . Sae, Fuel Cell Hybrid Propulsion Challenges and Opportunities for Commercial Aviation, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010.
DOI : 10.2514/6.2010-6537

J. Thauvin, G. Barraud, X. Roboam, B. Sareni, M. Budinger et al., Hybrid propulsion for regional aircraft: A comparative analysis based on energy efficiency, 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC), 2016.
DOI : 10.1109/ESARS-ITEC.2016.7841392
URL : https://hal.archives-ouvertes.fr/hal-01413276

M. Armstrong, C. Ross, D. Phillips, and M. Blackwelder, Stability, Transient Response, Control, and Safety of a High-Power Electric Grid for Turboelectric Propulsion of Aircraft, 2013.

A. V. Petrov, Aerodynamics of STOL Airplanes with Powered High-Lift Systems, 28 th International Congress of the Aeronautical Science, ICAS, 2012.

A. M. Stoll, Comparison of CFD and Experimental Results of the LEAPTech Distributed Electric Propulsion Blown Wing, 15th AIAA Aviation Technology, Integration, and Operations Conference, 2015.
DOI : 10.2514/6.2015-3188

M. D. Patterson, J. M. Derlaga, and N. K. Borer, High-Lift Propeller System Configuration Selection for NASA's SCEPTOR Distributed Electric Propulsion Flight Demonstrator, 16th AIAA Aviation Technology, Integration, and Operations Conference, 2009.
DOI : 10.2514/6.2016-3922

A. Dubois, M. Geest, J. Bevirt, S. Clarke, R. J. Christie et al., Design of an Electric Propulsion System for SCEPTOR Design Studies of Thin-Haul Commuter Aircraft with Distributed Electric Propulsion Preliminary Experimental Assessment of the Boundary Layer Ingestion Benefit for the D8 Aircraft A Multidisciplinary Optimization Method for Designing Boundary Layer Ingesting Inlets, 16 th AIAA Aviation Technology, Integration, and Operations Conference 16 th AIAA Aviation Technology, Integration, and Operations Conference 52 nd Aerospace Sciences Meeting, 2014.