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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Beck, Walter	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Henne, Ulrich	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Hirschen, Christian	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2013

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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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