Robert Konrath

发表

Development & Application of modern Measurement Techniques for pressurised cryogenic Wind Tunnels

Uwe Fey, Jürgen Quest, Janin Leuckert, 2008 .

Common research on large-scale wing wake vortices using PIV in the free flight laboratory B20

Jürgen Kompenhans, Andreas Schröder, Jean-Claude Monnier, 2010 .

High-Speed PIV Applied to Wake of NASA CRM Model in ETW Under High Re-Number Stall Conditions for Sub- and Transonic Speeds

Jürgen Quest, Robert Konrath, Reinhard Geisler, 2015 .

Flow Field Measurements by PIV at High Reynolds Numbers

Jürgen Quest, Robert Konrath, Eric Roosenboom, 2013 .

Experiences from Flow Field Measurements in Industrial Transonic Wind Tunnels for Comparison with Numerical Results

Jürgen Kompenhans, Andreas Schröder, Christian Klein, 2005 .

Flow Field Investigations on the SACCON Configuration in Stationary and Pitching Mode by Means of Particle Image Velocimetry

Andreas Schröder, Robert Konrath, Eric Roosenboom, 2011 .

Tracking the Nacelle Vortex Above Aircraft Wing in the ETW at Real Mach- and Reynolds Numbers by Means of PIV

Jürgen Quest, Robert Konrath, Reinhard Geisler, 2015 .

Recent Applications of Particle Image Velocimetry for Investigation of Unsteady Flow Fields in Industrial Transonic Wind Tunnels

Jürgen Kompenhans, Andreas Schröder, Robert Konrath, 2005 .

Development of Particle Image Velocimetry for In-Flight Flow Measurement

Andreas Schröder, Robert Konrath, Janos Agocs, 2013 .

Developments of PIV in Aerodynamics

Dirk Michaelis, Jürgen Kompenhans, Christian Willert, 2010 .

Formation Flight of Low-Aspect-Ratio Wings at Low Reynolds Number

Robert Konrath, Ivan Korkischko, I. Korkischko, 2017 .

Advanced Measurement Techniques for High Reynolds Number Testing in Cryogenic Wind Tunnels

Jürgen Kompenhans, Uwe Fey, Robert Konrath, 2010 .

Experimental investigations on the VFE-2 configuration at DLR, Göttingen, Germany; In Understanding and Modelling Vortical Flows to Improve the Technology Readiness Level for Military Aircraft

Andreas Schröder, Klaus Groot de, Robert Konrath, 2009 .

Dynamics and decay of spatially-evolving two- and four-vortex wakes near the ground

Robert Konrath, Roger Cocle, O. Desenfans, 2008 .

Analysis of PSP Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds

Jürgen Kompenhans, Andreas Schröder, Robert Konrath, 2006 .

Wing Wake Measurements at High Reynolds Numbers by Means of Cryo PIV

Jürgen Quest, Robert Konrath, Eric Roosenboom, 2013 .

Adaptation of PIV for Application in Cryogenic Pressurized Wind Tunnel Facilities at High Reynolds Numbers

Jürgen Kompenhans, Uwe Fey, Jürgen Quest, 2010 .

In-Flight Flow Visualisation Using Particle Image Velocimetry

Jürgen Kompenhans, Andreas Schröder, Robert Konrath, 2010 .

- Particle Image Velocimetry - Development and Certification of a Promising Tool for In-Flight Flow Flied Measurements

Andreas Schröder, Robert Konrath, Fritz Boden, 2010 .

Experimental and numerical investigations of pitch-plunging wing aerodynamics at low Reynolds number

Rolf Radespiel, Robert Konrath, Hauke Ehlers, 2013 .

PIV for complex high-lift-configurations

Andreas Schröder, Robert Konrath, Janos Agocs, 2006 .

Wake vortex alleviation by differential and oscillating flap settings: A numerical and experimental study

Robert Konrath, Carl F. v. Carmer, Guido Voß, 2008 .

High resolution wing shape measurements of free flying birds

Thomas Wolf, Robert Konrath, Tania Kirmse, 2010 .

Investigations of strake wake vortices in a high-lift-configuration using Stereo-PIV

Andreas Schröder, Robert Konrath, Janos Agocs, 2005 .

Advanced Measurement Techniques for Cryogenic Testing

Jürgen Kompenhans, Christian Klein, Uwe Fey, 2008 .

Vortical flow investigations of a static and dynamic UCAV model using stereoscopic PIV

Andreas Schröder, Robert Konrath, Eric Roosenboom, 2010 .

Application of Pressure Sensitive Paint -Theory and Pratice-

Jürgen Kompenhans, Ulrich Henne, Christian Klein, 2006 .

Modern optical methods for the investigation of flows in aerodynamics

Jürgen Kompenhans, Christian Klein, Uwe Fey, 2006 .

3D Flow Field Investigations on Flapping Wing Aerodynamics

Rolf Radespiel, Robert Konrath, Hauke Ehlers, 2014 .

Validation experiment with 4-vortex wake in large tow tank (FAR-Wake Subtask 1.2.2)

Robert Konrath, Carl F. v. Carmer, 2008 .

Three-Dimensional Flow Field Investigations on Pitching Low Aspect Ratio Wings at Low Reynolds Numbers

Christian Willert, Robert Konrath, Reinhard Geisler, 2013 .

Simultaneous Measurements of Unsteady Aerodynamic Loads, Flow Velocity Fields, Position and Wing Deformations of MAVs in Plunging Motion

Jürgen Kompenhans, Rolf Radespiel, Robert Konrath, 2010 .

Particle Image Velocimetry for In-Flight Application- Preparation, Test and Lessons Learned -

Andreas Schröder, Robert Konrath, Fritz Boden, 2010 .

Going for Experimental and Numerical Unsteady Wake Analyses Combined with Wall Interference Assessment by Using the NASA CRM Model in ETW

Jürgen Quest, Robert Konrath, Thorsten Lutz, 2013 .

MEASURING SHAPE OF BIRD WINGS DURING FLIGHT USING AN OPTICAL CORRELATION BASED METHOD

Jürgen Kompenhans, Thomas Wolf, Robert Konrath, 2010 .

Influence of Renolds number on generation and decay of aircraft wakes: Experimental investigation using generic models, F13 and F13X

Robert Konrath, Carl F. v. Carmer, 2007 .

High-speed PIV applied to the wake of the NASA CRM model in ETW at high Re-number stall conditions for sub- and transonic speeds

Jürgen Quest, Robert Konrath, Reinhard Geisler, 2015 .

Chapter 1 – Static and Dynamic SACCON PIV Tests - Part II: Aft Flow Field

Andreas Schröder, Robert Konrath, Eric Roosenboom, 2010 .

Measuring Shape of Bird Wings During Free Flapping Flight Using an Optical Method

Thomas Wolf, Robert Konrath, Thomas Wolf, 2012 .

High-speed PIV applied to wake of NASA CRM model at high Re-number sub- and transonic stall conditions

Jürgen Quest, Robert Konrath, Reinhard Geisler, 2018 .

Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration

Ulrich Henne, Christian Klein, Werner Sachs, 2006 .

Stereoscopic Particle Image Velocimetry Flowfield Investigation of an Unmanned Combat Air Vehicle

Jean-Claude Monnier, Anne Gilliot, Andreas Schröder, 2012 .

Wake vortex alleviation by differential and oscillating flap setting: a comparative numerical and experimental study

Eike Stumpf, Robert Konrath, Carl F. v. Carmer, 2007 .

Flow Field Investigations on a UCAV with a Ducted Engine Air Intake at Transonic Conditions

Robert Konrath, Eric Roosenboom, Janos Agocs, 2013 .

Developments for Industrial PIV

Dirk Michaelis, Jürgen Kompenhans, Christian Willert, 2009 .

Impact of Turbulence and Ground on Wake Vortex Evolution- Towing Tank Studies

Robert Konrath, Reinhard Geisler, Janos Agocs, 2012 .

Application of Stereo PIV to the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds

Jürgen Kompenhans, Andreas Schröder, Robert Konrath, 2006 .

Investigation of wake vortics in a water towing tank

Robert Konrath, Reinhard Geisler, Janos Agocs, 2011 .

Planned experimental investigations on a MAV model with rigid as well as with flexible wings

Robert Konrath, 2007 .

Numerical studies of the vortical flow around delta wing with rounded leading edges in comparison to experimental data within the Vortex Flow Experiment (VFE-2)

Heinrich Lüdeke, Robert Konrath, Andreas Schütte, 2007 .

Looking at owls from two angles; A study of wing anatomy of the barn owl Tyto alba with two different multi camera systems

Thomas Wolf, Robert Konrath, Hermann Wagner, 2011 .

Accepting a Challenge -The Development of PIV for Application in pressurized cryogenic Wind Tunnels

Jürgen Quest, Robert Konrath, J. Quest, 2011 .

Time Resolved Flow Field Investigations of Low Reynolds number Transient Maneuvers

Rolf Radespiel, Robert Konrath, Hauke Ehlers, 2016 .

Applications of Particle Image Velocimetry to industrial aerodynamic research

Jürgen Kompenhans, Christian Willert, Michaela Herr, 2009 .

Proposal for a combined PSP measurement in DNW-TWG: Intensity technique by DLR and Lifetime technique by AEDC

Christian Klein, Robert Konrath, Marvin Sellers, 2006 .

Recent Developments of Image Based Measurement Methods for Application to Transonic Flows in Industrial Wind Tunnels

Jürgen Kompenhans, Ulrich Henne, Uwe Fey, 2006 .

The projected pattern correlation technique for vibration measurements

U. Fuellekrug, Robert Konrath, Juergen Kompenhans, 2004, International Conference on Vibration Measurements by Laser Techniques: Advances and Applications.

Towing tank investigations on 2- and 4-vortex systems in ground effect using PIV

Robert Konrath, Carl F. v. Carmer, 2008 .

High lift flow structures: In-flight PIV feasibility study

Andreas Schröder, Robert Konrath, Fritz Boden, 2009 .

Aerodynamic measurement technology

Christian Klein, Robert Konrath, Walter Beck, 2006 .

Vortical flow field investigations on a stationary and pitching UCAV model using PIV

Andreas Schröder, Robert Konrath, Eric Roosenboom, 2010 .

PSP and PIV investigations on the VFE-2 configuration in sub- and transonic flow

Christian Klein, Andreas Schröder, Robert Konrath, 2008 .

Evaluation of Large-Scale Wing Vortex Wakes from Multi-Camera PIV Measurements in Free-Flight Laboratory

Jean-Claude Monnier, Anne Gilliot, Andreas Schröder, 2007 .

PSP and PIV Investigations on the VFE-2 Configuration in Sub- and Transonic Flow

Christian Klein, Andreas Schröder, Robert Konrath, 2008 .

Identification of vortex pairs in aircraft wakes from sectional velocity data

Jean-Claude Monnier, Andreas Schröder, Robert Konrath, 2008 .

Analysis of PSP Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds

Christian Klein, Robert Konrath, Dirk Otter, 2006 .

Analysis of Flow Field Measurements Obtained in a Large Tow Tank Regarding the Decay of Wake Vortices in the Far-Field for Two- and Four-Vortex Systems

Robert Konrath, Carl F. v. Carmer, Dieter Pallek, 2009 .

Progress in Optical Measurement Methods in Cryogenic Conditions

Ulrich Henne, Jürgen Quest, Robert Konrath, 2013 .

Avian wing geometry and kinematics of a free-flying barn owl in flapping flight

Robert Konrath, Thomas Wolf, Thomas Wolf, 2015 .

Enhancement of aircraft wake vortex decay in ground proximity

Takashi Misaka, Robert Konrath, Reinhard Geisler, 2014 .

Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing

Jürgen Kompenhans, Christian Klein, Andreas Schröder, 2008 .