Diekmann, Jobst Henning und Keller, Dennis und Edris, Faez und Ralf, Rudnik und Volker, Gollnick (2017) Flight mechanics model for spanwise lift and rolling moment distributions of a segmented active high-lift wing. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-017-0261-4. ISSN 1869-5590.
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Offizielle URL: https://link.springer.com/article/10.1007/s13272-017-0261-4
Kurzfassung
In this study, the aerodynamics of wings using an active high-lift system are investigated. The target is the flight mechanical description of the spanwise forces and resulting moments and the influence of the active high-lift system to their distribution. The high-lift system is a blown flap system divided into six segments per wing. Each segment is assumed to be individually controlled, so the system shall be used for aircraft control and system failure management. This work presents a flight mechanical sub-model for the simulation of flight dynamics, which has been derived from high-fidelity CFD results. An assessment of single-segment blowing system failures will be presented including recommendations for compensation of either lift or rolling moment loss. For this investigation, the compensation is required to act at the same wing side on which the failure appears. Thus, the potential for an increase of system reliability shall be proven. The results show that less performance investment in terms of pressurized air is necessary to compensate the rolling moment of a failing segment instead of its lift. However, large blowing performance increases for the remaining wing segments that occur for some of the failure cases.
elib-URL des Eintrags: | https://elib.dlr.de/114344/ | ||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||
Titel: | Flight mechanics model for spanwise lift and rolling moment distributions of a segmented active high-lift wing | ||||||||||||||||||||||||
Autoren: |
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Datum: | 21 September 2017 | ||||||||||||||||||||||||
Erschienen in: | CEAS Aeronautical Journal | ||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
DOI: | 10.1007/s13272-017-0261-4 | ||||||||||||||||||||||||
Verlag: | Springer | ||||||||||||||||||||||||
ISSN: | 1869-5590 | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Active high-lift, Coandă flaps, Flight dynamics model, Short take-off and landing, Spanwise lift distribution, Aircraft control | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation und Validierung (alt), L - Flugphysik (alt) | ||||||||||||||||||||||||
Standort: | Braunschweig | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Flugsystemtechnik > Flugdynamik und Simulation Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge Lufttransportsysteme | ||||||||||||||||||||||||
Hinterlegt von: | Diekmann, Dr. Jobst Henning | ||||||||||||||||||||||||
Hinterlegt am: | 11 Okt 2017 15:27 | ||||||||||||||||||||||||
Letzte Änderung: | 08 Mär 2018 19:01 |
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- Flight mechanics model for spanwise lift and rolling moment distributions of a segmented active high-lift wing. (deposited 11 Okt 2017 15:27) [Gegenwärtig angezeigt]
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