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Application of PSP up to Mach 4

Engler, R. (2004) Application of PSP up to Mach 4. DLR/ONERA - Annex II Meeting, DLR, Köln, 6. - 7. April 2004.

Full text not available from this repository.

Abstract

Using the mobile DLR PSP-System and DLR02 paint in a two days test principle investigations were performed for different pressure ratios (100 to 320) between the test section and the RCS to check the usability in such type of flows. After some test runs to check the principal function and strong enough paint and its good contact to the models surface, various objects were investigated at different flow speeds and temperatures. Especially on a rocket model the reaction control system (RCS) was investigated in detail for angles of attack around 15° and surface temperatures of -10°C to -20°C. A detailed pressure distribution around the nozzle in the middle cylindrical part of the model could be visualized and quantitative calculated as well as compared with conventional pressure taps.

Item URL in elib:https://elib.dlr.de/12812/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Application of PSP up to Mach 4
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Engler, R.UNSPECIFIEDUNSPECIFIED
Date:2004
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:1-
Status:Published
Keywords:PSP-System, Mach numbers
Event Title:DLR/ONERA - Annex II Meeting, DLR, Köln, 6. - 7. April 2004
Organizer:DLR/ONERA
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: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Micknaus, Ilka
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:32

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