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Gardner, Anthony Donald (2006) Investigation of the sting interference effect due to the TWG 15-degree, 25-degree and 45-degree rolling stings. DLR-Interner Bericht. IB 2006 A 32. 234 S.
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Abstract
This report details a series of numerical experiments designed to provide an assessment of the acceptable sting length between the model and the sting holder required to minimise sting interference for the TWG 15-degree, 25-degree and 45-degree rolling stings. Calculations were undertaken for Mach numbers of 0.50, 0.90, 1.05 and 1.63, and for model attitudes between 0 and 55 degrees. These calculations indicated that the minimum spacing varied with the Mach number and angle of attack between 1 cm and 20 cm.
| Item URL in elib: | https://elib.dlr.de/44435/ | ||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||
| Title: | Investigation of the sting interference effect due to the TWG 15-degree, 25-degree and 45-degree rolling stings. | ||||||
| Authors: |
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| Date: | 2006 | ||||||
| Refereed publication: | No | ||||||
| Open Access: | No | ||||||
| Gold Open Access: | No | ||||||
| In SCOPUS: | No | ||||||
| In ISI Web of Science: | No | ||||||
| Number of Pages: | 234 | ||||||
| Status: | Published | ||||||
| Keywords: | CFD, TAU, support interference, TWG | ||||||
| HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||
| 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: | Göttingen | ||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > High Speed Configurations | ||||||
| Deposited By: | Gardner, Dr.habil. Anthony | ||||||
| Deposited On: | 20 Jun 2007 | ||||||
| Last Modified: | 27 Apr 2009 13:01 |
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