Numerical flow simulations of a propeller design for an eVTOL vehicle using the Vortex Particle Method

Guignard, Thomas (2025) Numerical flow simulations of a propeller design for an eVTOL vehicle using the Vortex Particle Method. Student thesis, Sigma Clermont.

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Item URL in elib:

https://elib.dlr.de/222756/

Document Type:

Thesis (Student thesis)

Title:

Numerical flow simulations of a propeller design for an eVTOL vehicle using the Vortex Particle Method

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Guignard, Thomas	thomas.guignard (at) dlr.de	UNSPECIFIED	UNSPECIFIED

DLR Supervisors:

Contribution	DLR Supervisor	Institution or E-Mail	DLR Supervisor's ORCID iD
Thesis advisor	Guerin, Sebastien	Sebastien.Guerin (at) dlr.de	UNSPECIFIED
Thesis advisor	Lade, Tobias	tobias.lade (at) dlr.de	https://orcid.org/0009-0008-1608-9296

Date:

2025

Open Access:

Yes

Number of Pages:

Status:

Published

Keywords:

VPM, eVTOL

Institution:

Sigma Clermont

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Clean Propulsion

DLR - Research area:

Aeronautics

DLR - Program:

L CP - Clean Propulsion

DLR - Research theme (Project):

L - Virtual Engine

Location:

Berlin-Charlottenburg

Institutes and Institutions:

Institute of Propulsion Technology > Engine Acoustic

Deposited By:

Guerin, Sebastien

Deposited On:

11 Feb 2026 11:43

Last Modified:

11 Feb 2026 19:44

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