Klein, Christian (2008) Recent Developments of PSP and TSP at DLR for Application to Transonic Flows in Industrial Wind Tunnels. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, NV (USA). ISBN 978-1-56347-937-3.
Full text not available from this repository.
Official URL: http://www.aiaa.org
Abstract
The pressure sensitive paint (PSP system is an optical measurement technique to investigate absolute pressure fields on model surfaces for basic research in laboratories, industrial wind tunnels or high speed rotating turbo machines. Detailed qualitative and quantitative information and understanding of flow phenomena can be obtained in speed ranges from U∞ =20 m/s up to Ma= 5.0. A number of investigations of problems of industrial interest in different speed ranges from low speed flow over transonic to trisonic and cryogenic flows have been realised and compared with conventional techniques like point wise pressure measurements, flow velocity field measurements (PIV), and qualitative visualization (laser light sheets). The influences of the main error sources for the components of the PSP system have been checked. Comparison of experimental pressure fields obtained by means of PSP and the results of numerical calculations have been carried out. Different wind tunnel models ranging from basic configurations such as a cropped delta wing to a complex half model of a large propeller-driven transport aircraft with all flaps, rudders and shrouds, and rotating or oscillating models as well as Reynolds number effects by means of TSP on models have been investigated.
Item URL in elib: | https://elib.dlr.de/50700/ | ||||||||
---|---|---|---|---|---|---|---|---|---|
Document Type: | Conference or Workshop Item (Speech) | ||||||||
Additional Information: | 2008 AIAA Meeting Papers on Disc, Vol. 13, No. 1 (ASM) Conference Proceeding Series Published by AIAA, © 2008, DVD-ROM ISBN-10: 1-56347-937-0 | ||||||||
Title: | Recent Developments of PSP and TSP at DLR for Application to Transonic Flows in Industrial Wind Tunnels | ||||||||
Authors: |
| ||||||||
Date: | 2008 | ||||||||
Refereed publication: | No | ||||||||
Open Access: | No | ||||||||
Gold Open Access: | No | ||||||||
In SCOPUS: | No | ||||||||
In ISI Web of Science: | No | ||||||||
Volume: | Vol. 13 | ||||||||
Page Range: | 33Folien | ||||||||
Series Name: | 2008 AIAA Meeting Papers on Disc (DVD-ROM) | ||||||||
ISBN: | 978-1-56347-937-3 | ||||||||
Status: | Published | ||||||||
Keywords: | Optical pressure measurement, pressure sensitive Paint, PSP, temperature sensitive paint, TSP, optical sensors | ||||||||
Event Title: | 46th AIAA Aerospace Sciences Meeting and Exhibit | ||||||||
Event Location: | Reno, NV (USA) | ||||||||
Event Type: | international Conference | ||||||||
Event Start Date: | 7 January 2008 | ||||||||
Event End Date: | 10 January 2008 | ||||||||
Organizer: | AIAA | ||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||
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 > Experimental Methods | ||||||||
Deposited By: | Micknaus, Ilka | ||||||||
Deposited On: | 04 Oct 2007 | ||||||||
Last Modified: | 24 Apr 2024 19:13 |
Repository Staff Only: item control page