Inac, Hilal and Schwarz, Thorsten (2024) Validation of a turbulent boundary layer method for fuselages of helicopters. 24th joint ONERA-DLR Aerospace Smyposium, 2024-06-12 - 2024-06-14, Braunschweig, Germany.
|
PDF
- Only accessible within DLR until January 2027
1MB |
Abstract
In this paper the panel-freewake method UPM was extended with Truckenbrodts boundary layer method for predicting the viscous flow for non-lifting bodies. The newly implemented Truckenbrodts boundary layer analysis is validated for the helicopter fuselage of DLRs FastRescue project.
| Item URL in elib: | https://elib.dlr.de/210548/ | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||
| Title: | Validation of a turbulent boundary layer method for fuselages of helicopters | ||||||||||||
| Authors: |
| ||||||||||||
| Date: | June 2024 | ||||||||||||
| Refereed publication: | No | ||||||||||||
| Open Access: | No | ||||||||||||
| Gold Open Access: | No | ||||||||||||
| In SCOPUS: | No | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| Status: | Published | ||||||||||||
| Keywords: | panel-freewake method, UPM, boundary layer method, lifting bodies, non-lifting bodies, fuselage, Truckenbrodt, helicopter | ||||||||||||
| Event Title: | 24th joint ONERA-DLR Aerospace Smyposium | ||||||||||||
| Event Location: | Braunschweig, Germany | ||||||||||||
| Event Type: | Workshop | ||||||||||||
| Event Start Date: | 12 June 2024 | ||||||||||||
| Event End Date: | 14 June 2024 | ||||||||||||
| Organizer: | ONERA and DLR | ||||||||||||
| 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 09:46 | ||||||||||||
| Last Modified: | 12 Dec 2024 09:46 |
Repository Staff Only: item control page