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van der Wall, Berend G. (2013) Representation of Yaw Angle Influence on the Fuselage-Induced Velocities in the Rotor Disk. DLR-Interner Bericht. DLR-IB 111-2013/31. DLR Institut für Flugsystemtechnik. 42 S.
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Abstract
An analytical mathematical model is developed to compute fuselage-induced velocities in the volume of a helicopter rotor operation for use in comprehensive rotor codes, prescribed and free-wake codes.
| Item URL in elib: | https://elib.dlr.de/83902/ | ||||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||||
| Title: | Representation of Yaw Angle Influence on the Fuselage-Induced Velocities in the Rotor Disk | ||||||||
| Authors: |
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| Date: | 30 August 2013 | ||||||||
| Refereed publication: | No | ||||||||
| Open Access: | No | ||||||||
| Number of Pages: | 42 | ||||||||
| Status: | Published | ||||||||
| Keywords: | helicopter simulation, helicotper aerodynamics, interactional aerodynamics, rotor-fuselage interaction | ||||||||
| Institution: | DLR Institut für Flugsystemtechnik | ||||||||
| Department: | Hubschrauber | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | Rotorcraft (old) | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L RR - Rotorcraft Research | ||||||||
| DLR - Research theme (Project): | L - The Innovative Rotorcraft (old) | ||||||||
| Location: | Braunschweig | ||||||||
| Institutes and Institutions: | Institute of Flight Systems > Rotorcraft | ||||||||
| Deposited By: | van der Wall, Prof. Dr. Berend G. | ||||||||
| Deposited On: | 09 Sep 2013 15:01 | ||||||||
| Last Modified: | 09 Sep 2013 15:01 |
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