Keller, Dennis (2013) Numerical Investigation of Engine Effects on the Stability and Controllability of a Transport Aircraft with Circulation Control. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego, USA.
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Abstract
The scope of this paper is to illustrate the installation effects of a turboprop engine on a high-lift configuration of a short take off and landing (STOL) aircraft with circulation control. In addition to the influence on the wing performance, the impact on the longitudinal static stability of the whole aircraft is also investigated. Furthermore, critical failure cases, namely one engine inoperative (OEI), as well as an asymmetric circulation control failure are assessed. Therefore, CFD calculations based on the Reynolds-averaged Navier-Stokes (RANS) equations were performed, whereas the propeller is modeled with an actuator disk.
Item URL in elib: | https://elib.dlr.de/84479/ | ||||||
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Document Type: | Conference or Workshop Item (Speech) | ||||||
Title: | Numerical Investigation of Engine Effects on the Stability and Controllability of a Transport Aircraft with Circulation Control | ||||||
Authors: |
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Date: | 1 June 2013 | ||||||
Refereed publication: | No | ||||||
Open Access: | No | ||||||
Gold Open Access: | No | ||||||
In SCOPUS: | No | ||||||
In ISI Web of Science: | No | ||||||
Status: | Published | ||||||
Keywords: | Aerodynamics Flight Dynamics Circulation Control CFD | ||||||
Event Title: | 31st AIAA Applied Aerodynamics Conference | ||||||
Event Location: | San Diego, USA | ||||||
Event Type: | international Conference | ||||||
Event Dates: | 24.-27. Juni 2013 | ||||||
Organizer: | AIAA | ||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||
HGF - Program: | Aeronautics | ||||||
HGF - Program Themes: | Aircraft Research (old) | ||||||
DLR - Research area: | Aeronautics | ||||||
DLR - Program: | L AR - Aircraft Research | ||||||
DLR - Research theme (Project): | L - Flight Physics (old) | ||||||
Location: | Braunschweig | ||||||
Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Transport Aircraft | ||||||
Deposited By: | Keller, Dennis | ||||||
Deposited On: | 16 Oct 2013 09:18 | ||||||
Last Modified: | 08 May 2014 23:18 |
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