Schröder, W. (1998) Determination of the suction velocities for the boundary layer stability analysis of the first fifteen ELFIN II wing test cases. Project Report, DLR-Interner Bericht. 129-98/17.
Full text not available from this repository.
Abstract
In preparation for the laminar boundary layer stability analysis of the first 15 selected test runs of the ELFIN II HLF half wing test program in S1MA (Nov. 1996) the suction velocities have been assessed. They are based on the suction panel loss characteristics of the half wing as measured by DLR in October 1997 at DASA site Varel. The suction velocities are provided for the same chordwise positions as the surface pressures interpolated by BAe, which completes the input for the final boundary layer stability calculations.
Item URL in elib: | https://elib.dlr.de/13081/ | ||||||||
---|---|---|---|---|---|---|---|---|---|
Document Type: | Monograph (Project Report, DLR-Interner Bericht) | ||||||||
Additional Information: | LIDO-Berichtsjahr=1999, | ||||||||
Title: | Determination of the suction velocities for the boundary layer stability analysis of the first fifteen ELFIN II wing test cases | ||||||||
Authors: |
| ||||||||
Date: | 1998 | ||||||||
Open Access: | No | ||||||||
Status: | Published | ||||||||
Keywords: | Grenzschicht-Stabilität, Laminare Grenzschicht, HLF Stability, Grenzschichtabsaugung | ||||||||
HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||
HGF - Program: | Aeronautics | ||||||||
HGF - Program Themes: | other | ||||||||
DLR - Research area: | Aeronautics | ||||||||
DLR - Program: | L ST - Starrflüglertechnologien | ||||||||
DLR - Research theme (Project): | L - Concepts & Integration (old) | ||||||||
Location: | Köln-Porz , Braunschweig , Göttingen | ||||||||
Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik | ||||||||
Deposited By: | Grant, Claudia | ||||||||
Deposited On: | 16 Sep 2005 | ||||||||
Last Modified: | 14 Jan 2010 19:56 |
Repository Staff Only: item control page