Application of Pressure Sensitive Paint for determination of the pressure field of aircraft models in wind tunnels

Klein, Christian (2008) Application of Pressure Sensitive Paint for determination of the pressure field of aircraft models in wind tunnels. XIX Biannual Symposium on Measuring Techniques in Turbomachinery, 2008-04-07 - 2008-04-08, Sint Genesius Rode (Belgium).

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/54154/

Document Type:

Conference or Workshop Item (Speech)

Additional Information:

Folien

Title:

Application of Pressure Sensitive Paint for determination of the pressure field of aircraft models in wind tunnels

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Klein, Christian	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2008

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Page Range:

pp. 1-19

Series Name:

Conference Proceedings

Status:

Published

Keywords:

Pressure Sensitive Paint (PSP), binary paint

Event Title:

XIX Biannual Symposium on Measuring Techniques in Turbomachinery

Event Location:

Sint Genesius Rode (Belgium)

Event Type:

international Conference

Event Start Date:

7 April 2008

Event End Date:

8 April 2008

Organizer:

von Karman Institute for Fluid Dynamics

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:

11 Jun 2008

Last Modified:

24 Apr 2024 19:17

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