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Schütte, Andreas and Puttur, Anirvin (2025) Pitch Recovery Investigations on a Generic Fighter Aircraft Configuration. DLR.
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Abstract
The presented investigations analyses the vortical flow physics and aerodynamic performance of DLR-FFD 2nd Gen. aircraft configuration. The work focuses on the aerodynamic task to determine the pitching moment performance and in particular the ability to provide the requested pitch recovery moment. The numerical investiga-tions have been performed with the DLR RANS solver TAU
| Item URL in elib: | https://elib.dlr.de/222761/ | ||||||||||||
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| Document Type: | Editorship of Proceedings | ||||||||||||
| Title: | Pitch Recovery Investigations on a Generic Fighter Aircraft Configuration | ||||||||||||
| Authors: |
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| Date: | 12 October 2025 | ||||||||||||
| Refereed publication: | No | ||||||||||||
| Open Access: | No | ||||||||||||
| Gold Open Access: | No | ||||||||||||
| In SCOPUS: | No | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| Publisher: | DLR | ||||||||||||
| Status: | Published | ||||||||||||
| Keywords: | CFD, Aircraft Design, Fighter Aircraft, Vortical Flows | ||||||||||||
| HGF - Research field: | other | ||||||||||||
| HGF - Program: | other | ||||||||||||
| HGF - Program Themes: | other | ||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||
| DLR - Program: | L DT - Defense Technology | ||||||||||||
| DLR - Research theme (Project): | L - Effect | ||||||||||||
| Location: | Braunschweig | ||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Transport Aircraft | ||||||||||||
| Deposited By: | Schütte, Andreas | ||||||||||||
| Deposited On: | 09 Mar 2026 08:28 | ||||||||||||
| Last Modified: | 09 Mar 2026 08:28 |
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