DESIGN OF A DISTRIBUTED PROPULSION CONCEPT USING AN ADJOINT-BASED APPROACH AND BLADE ELEMENT THEORY TO MINIMIZE POWER

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Bibliographische Detailangaben
Veröffentlicht in:	AIAA Aviation Forum (2020 : Online) Aircraft design
1. Verfasser:	Ordaz, Irian (VerfasserIn)
Weitere Verfasser:	Nielsen, Eric J. (VerfasserIn), Wang, Li (VerfasserIn)
Format:	UnknownFormat
Sprache:	eng
Veröffentlicht:	2020
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