Sustainable aircraft design — A review on optimization methods for electric propulsion with derived optimal number of propulsors-Reference-Cited by-同舟云学术

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Sustainable aircraft design — A review on optimization methods for electric propulsion with derived optimal number of propulsors

Published:2021-05 Issue: Volume:123 Page:100714
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Pelz Peter F.,Leise Philipp,Meck Marvin

Funder

Deutsche Forschungsgemeinschaft

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference206 articles.

1. European Aviation Environmental Report;European Union Aviation Safety Agency,2019

2. Turboelectric distributed propulsion engine cycle analysis for hybrid-wing-body aircraft;Felder,2009

3. Think:Act Aircraft Electrical Propulsion - Onwards and Upwards;Berger,2018

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1. Aerodynamic simulations of an electric vertical takeoff and landing aircraft using reformulated vortex particle method;Physics of Fluids;2024-06-01

2. Numerical Simulation and Experimental Study on the Aerodynamics of Propulsive Wing for a Novel Electric Vertical Take-Off and Landing Aircraft;Aerospace;2024-05-27

3. Grand challenges in aerospace engineering;Frontiers in Aerospace Engineering;2024-03-04

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