DESIGN OF A DISTRIBUTED PROPULSION CONCEPT USING AN ADJOINT-BASED APPROACH AND BLADE ELEMENT THEORY TO MINIMIZE POWER
AIAA Aviation Forum ; 2020 ; Online
2020
Conference paper
English
BKL: | 55.50 Luftfahrzeugtechnik |
AIAA-2019-3681: Adjoint-Based Design of a Distributed Propulsion Concept with a Power Objective
British Library Conference Proceedings | 2019
|