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Department Experimental Methods (AS-EXV)

Göttingen

Particle Image Velocimetry in DNW-TWG
.
360°-PSP measurement in DNW-HST
.
Flap gap measurement of an AIRBUS A340
.
Acoustic source map of a Dornier DO-728 half model in DNW-KKK

The Department of Experimental Methods develops optical and acoustical field measurement techniques for the acquisition of fluid-mechanical and aero-acoustical quantities and applies them mainly in large industrial wind tunnels and at in-flight testing for aerodynamics.

Quantitatively measurable values are pressure (PSP), velocity (PIV), location of transition lines (TSP), density (BOS), and sound pressure (Acoustic Microphone Array), in parallel with the determination of deformation (IPCT, PROPAC) and position of the model in the wind tunnel or of the wing of an aircraft or of a propeller. Application is mainly performed in the scope of large industrial projects in European co-operation. For this purpose mobile measurement systems have been developed by the department, which can be flexibly adjusted to particular testing environments. The quality of the results obtained in the rough environment of industrial test facilities is comparable with the results attained in the laboratory of universities.

All data is acquired with high spatial and temporal resolution non-intrusively so that no interference of the flow field by the measurement is to occur. In consequence, the methods developed are particularly suited for the aero-dynamical and aero-acoustical analysis of complex, unsteady three-dimensional flow fields. The acquired data sets constitute a reliable basis for the validation of numerical codes.

Increasingly, these image based measurement techniques are applied in parallel to obtain a more complete description of the flow field by determining several physical quantities simultaneously.

Measurement techniques

  • for flow field analysis:  PIV, Tomo-PIV, BOS
  • for surface analysis: PSP, TSP, Position detection, EDT, Moiré-Interferometry, IPCT, PROPAC/REPAC
  • for sound field analysis: Phased Microphone Array
  • Non-standard Video Systems: High performance LED Illuminator, High-speed video stroboscope

Hard- and software products

  • Hard- and software developed by the department EXV

Projects

  • AIM² - Advanced In-flight Measurement Techniques 2
  • ALSA - Akustische Lokalisation von Strömungsablösung im ETW
  • AVERT
  • CREDO - Cabin noise Reduction by Experimental and numerical Design Optimization
  • EWA - European Windtunnel Association
  • FAR-Wake - Aircraft Wake Phenomena
  • FLIRET - Flight Reynolds Number Testing
  • MARS - Manipulation of Reynolds Stress for Separation Control and Drag Reduction
  • PivNet 2 - Particle Image Velocimetry for industrial applications
  • SAMURAI - Synergy of Advanced Measurement Techniques for Unsteady and High Reynolds Number Aerodynamic Investigations
  • SIMKAB
  • TELFONA - Testing for Laminar Flow on New Aircraft
  • VFE-2 - International Vortex Flow Experiment 2
  • X3NOISE

Conferences and courses

  • PIV Course, March 2013
  • PSP Course, September 2013
  • DGLR-Workshop: CFD and Experiment - Integration of Simulation, April 2011
  • 25 Years of PIV in Aerodynamics 

Awards

  • DLR Innovation Prize 2011 for the High Performance LED Illuminator
  • Best Movie Award: PIV analysis of L. Prandtl's historic flow visualization movies

Contact
Lars Koop
German Aerospace Center

Institute of Aerodynamics and Flow Technology
, Experimental Methods
Göttingen

Tel.: +49 551 709-2237

Fax: +49 551 709-2830

Catrin Rosenstock
Secretariat

German Aerospace Center

Institute of Aerodynamics and Flow Technology
, Experimental Methods
Göttingen

Tel.: +49 551 709-2461

Fax: +49 551 709-2830

Related Topics
Aerodynamic
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