English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Tools annual

Global: Zendy Free Plan

Global: Zendy Tools monthly

Global: Zendy Plus monthly

The development and spreading of electric aircrafts happen differently from what we would expect based on the electrification of automotive. Replacing the total combustionbased propulsion system to a fully electric drive system raises the need for optimization due to the energy efficiency. However, the mechanical and aerodynamical characteristics should be considered as well as the electrical in order to get a universal evaluation process. The aim of the present paper is to provide a method and metrics for energetic optimization during mission profile-oriented design of batteries. Therefore, more realistic claims can be raised against long-term electric aviation in terms of technical and also economical purposes.

Investigation of eAircraft energetic optimization