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Application of the Pressure Sensitive Paint (PSP) Technique to a Scramjet Nozzle Flow in the DLR Hypersonic Wind Tunnel H2K

Beck, Walter and Henne, Ulrich and Hirschen, Christian (2013) Application of the Pressure Sensitive Paint (PSP) Technique to a Scramjet Nozzle Flow in the DLR Hypersonic Wind Tunnel H2K. Seminar China Academy of Aerospace Aerodynamics (CAAA), 2013-08-13, Beijing, P.R. China.

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Item URL in elib:https://elib.dlr.de/83957/
Document Type:Conference or Workshop Item (Speech)
Title:Application of the Pressure Sensitive Paint (PSP) Technique to a Scramjet Nozzle Flow in the DLR Hypersonic Wind Tunnel H2K
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Beck, WalterUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Henne, UlrichUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hirschen, ChristianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:PSP; TSP; hypersonic facilities; short duration flows; pressures; temperatures
Event Title:Seminar China Academy of Aerospace Aerodynamics (CAAA)
Event Location:Beijing, P.R. China
Event Type:Other
Event Date:13 August 2013
Organizer:China Academy of Aerospace Aerodynamics (CAAA), Prof. Xue-Jun Zhao, NO. 17, Yungang West Road, Fengtai District, Beijing, P.R. China
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 - Simulation & Validation (old)
Location: Köln-Porz , Göttingen
Institutes and Institutions:German-Dutch Windtunnels
Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:04 Sep 2013 13:52
Last Modified:24 Apr 2024 19:50

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