Tell a friend
Print
Konrath, Robert and Geisler, Reinhard and Agocs, Janos and Ehlers, Hauke and Philipp, Florian and Quest, Jürgen (2018) High-Speed PIV Applied to wake of NASA CRM model at high Re-number sub- and transonic stall conditions. CEAS Aeronautical Journal, 9 (2), pp. 339-346. Springer. doi: 10.1007/s13272-017-0258-z. ISSN 1869-5582.
Full text not available from this repository.
Official URL: https://link.springer.com/article/10.1007/s13272-017-0258-z
Abstract
Within the framework of the EU project ESWIRP the Particle Image Velocimetry (PIV) using high-speed camera and laser has been used to measure the turbulent flow in the wake of a stalled aircraft wing. The measurements took place on the Common Research Model (CRM) provided by NASA in the pressurized cryogenic European Transonic Wind tunnel (ETW). A specific cryoPIV system has been used and adapted for using high-speed PIV components under the cryogenic conditions of the wind tunnel facility. First results are presented comprising transonic and subsonic stall conditions at realistic flight Reynolds numbers of 11.6 and 30 million, respectively.
| Item URL in elib: | https://elib.dlr.de/104849/ | ||||||||||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Document Type: | Article | ||||||||||||||||||||||||||||
| Additional Information: | Published online: 23 August 2017; Print ISSN: 1869-5582 ; Online ISSN: 1869-5590 | ||||||||||||||||||||||||||||
| Title: | High-Speed PIV Applied to wake of NASA CRM model at high Re-number sub- and transonic stall conditions | ||||||||||||||||||||||||||||
| Authors: |
| ||||||||||||||||||||||||||||
| Date: | June 2018 | ||||||||||||||||||||||||||||
| Journal or Publication Title: | CEAS Aeronautical Journal | ||||||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||||||||||
| Volume: | 9 | ||||||||||||||||||||||||||||
| DOI: | 10.1007/s13272-017-0258-z | ||||||||||||||||||||||||||||
| Page Range: | pp. 339-346 | ||||||||||||||||||||||||||||
| Editors: |
| ||||||||||||||||||||||||||||
| Publisher: | Springer | ||||||||||||||||||||||||||||
| Series Name: | Special Issue: Scientific Access to the European Strategic Wind Tunnels funded under the EU’s FP7-INFRASTRUCTURES grant 227816 | ||||||||||||||||||||||||||||
| ISSN: | 1869-5582 | ||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||
| Keywords: | PIV, ETW, Common Research model, High Reynolds Number, Wing Stall, Wing Wake | ||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Simulation and Validation (old) | ||||||||||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Experimental Methods, GO | ||||||||||||||||||||||||||||
| Deposited By: | Bachmann, Barbara | ||||||||||||||||||||||||||||
| Deposited On: | 13 Dec 2017 14:35 | ||||||||||||||||||||||||||||
| Last Modified: | 16 Sep 2025 04:13 |
Repository Staff Only: item control page
