Tell a friend
Print
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.
Full text not available from this repository.
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/ | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| 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: |
| ||||||||
| Date: | 2006 | ||||||||
| Refereed publication: | No | ||||||||
| Open Access: | 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 |
Repository Staff Only: item control page
