DLR Portal
Home
|
Textversion
|
Imprint
|
Sitemap
|
Contact
|
Deutsch
You are here:
Home
:
Departments
:
Turbine
:
The Probe Calibration Facility
Advanced Search
News
Institute
Departments
Combustor
Combustion Test
Fan and Compressor
Numerical Methods
Engine
Engine Acoustics
Engine Measurement
Turbine
Low Speed Cascade Tunnel (NGG)
Rotating Cascade Tunnel
The Probe Calibration Facility
The Straight Cascade Tunnel
Neuer Turbinenprüfstand NG-Turb
FACTOR
TFAST
Robustturb
AITEB-2
Adturb
IT Infrastruktur
Facilities
Publications
Offers
Service & Links
Back to article
Test section
Previous
2/3
Next
Downloads
The Behaviour of Probes in Transonic Flow Fields of Turbomachinery
(0.17 MB)
A New Test Facility for Probe Calibration - Offering Independent Variation of Mach and Reynolds Number
(0.8 MB)
Related Topics
Aerodynamic
Optics
Copyright © 2013 German Aerospace Center (DLR). All rights reserved.