Validation of a turbulent boundary layer method for fuselages of helicopters

Inac, Hilal and Schwarz, Thorsten (2024) Validation of a turbulent boundary layer method for fuselages of helicopters. 50th European Rotorcraft Forum 2024, 2024-09-10 - 2024-09-12, Marseille, France.

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Abstract

In this paper the panel-free wake method UPM was extended with Truckenbrodts boundary layer methods for predicting the viscous flow for non-lifting bodies

Item URL in elib:

https://elib.dlr.de/210508/

Document Type:

Conference or Workshop Item (Speech)

Title:

Validation of a turbulent boundary layer method for fuselages of helicopters

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Inac, Hilal	hilal.inac (at) dlr.de	UNSPECIFIED	UNSPECIFIED
Schwarz, Thorsten	Thorsten.Schwarz (at) dlr.de	https://orcid.org/0000-0003-1034-6120	UNSPECIFIED

Date:

September 2024

Refereed publication:

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

panel-free wake method, UPM, boundary layer, lifting bodies, non-lifting bodies, fuselage, Truckenbrodt, Stratford, helicopter

Event Title:

50th European Rotorcraft Forum 2024

Event Location:

Marseille, France

Event Type:

international Conference

Event Start Date:

10 September 2024

Event End Date:

12 September 2024

Organizer:

3AF

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Efficient Vehicle

DLR - Research area:

Aeronautics

DLR - Program:

L EV - Efficient Vehicle

DLR - Research theme (Project):

L - Virtual Rotorcraft and Validation

Location:

Braunschweig

Institutes and Institutions:

Institute for Aerodynamics and Flow Technology

Deposited By:

Inac, Hilal

Deposited On:

12 Dec 2024 09:42

Last Modified:

10 Sep 2026 03:00

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