Jürgen Quest

发表

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

Uwe Fey, Jürgen Quest, Janin Leuckert, 2008 .

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 .

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 .

Real-Flight Reynolds Number Microphone-Array Measurements on a Scaled Model in ETW

Thomas Ahlefeldt, Jürgen Quest, J. Quest, 2014 .

Slotted Wall Interference Investigation in ETW using the NASA CRM model

Jürgen Quest, S. M. Bosnyakov, S. V. Matyash, 2015 .

Hot-Wire Measurements in Cryogenic Environment

Jürgen Quest, Harald Quix, Christian Brzek, 2011 .

Flight Test Tailored ETW Testing of a Commercial Transport High Lift Configuration

Ralf Rudnik, Jürgen Quest, Matthias Schulz, 2015 .

Comparison of the NASA Common Research Model European Transonic Wind Tunnel test data to NASA National Transonic Facility test data

Melissa B. Rivers, Ralf Rudnik, Jürgen Quest, 2018 .

A short history of the European Transonic Wind Tunnel ETW

Jürgen Quest, John Green, J. Quest, 2011 .

Low Speed High Lift Validation Tests within the European Project EUROLIFT II

Matthias Schulz, Ralf Rudnik, Jürgen Quest, 2007 .

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 .

Advanced Design by Numerical Methods and Wind-Tunnel Verification Within European High-Lift Program

Domenico Quagliarella, Jochen Wild, Joel Brezillon, 2009 .

TOOLS AND TECHNIQUES FOR HIGH REYNOLDS NUMBER TESTING STATUS AND RECENT IMPROVEMENTS AT ETW

Jürgen Quest, Dieter Schimanski, J. Quest, 2003 .

Stall Behavior of the HINVA KH-A320-HA Highlift Model in ETW

Ralf Rudnik, Jürgen Quest, Niko Bier, 2015 .

Real-Flight Microphone-Array Measurements on a scaled Model in ETW

Thomas Ahlefeldt, Jürgen Quest, 2014 .

Applying numerical optimization to realistic high-lift design of transport aircraft – an overview of the aerodynamic design optimisation investigations within the EUROLIFT II project

Jochen Wild, Joel Brezillon, Jürgen Quest, 2005 .

Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW)

Uwe Fey, Jürgen Quest, Yasuhiro Egami, 2003, 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03..

Transonic High Reynolds Number Transition Experiments in the ETW Cryogenic Wind Tunnel

Uwe Fey, Raffaele Donelli, Jürgen Quest, 2010 .

TESTING OF A MODERN TRANSPORT AIRCRAFT CONFIGURATION IN ETW CLOSE TO MACH 0.9

Jürgen Quest, Airbus Uk, Stephen Rolston, 2002 .

Assessing Model Dynamics within the Critical Alpha Range

Jürgen Quest, Harald Quix, 2014 .

Complementary Numerical and Experimental Data Analysis of the ETW Telfona Pathfinder Wing Transition Tests

Stefan Hein, Uwe Fey, Jürgen Quest, 2011 .

THE ETW WALL INTERFERENCE ASSESSMENT FOR FULL AND HALF MODELS

Jürgen Quest, Norbert Gross, 2004 .

Doppler global velocimetry measurements in the European Transonic Windtunnel

Christian Willert, Jürgen Quest, Richard Schodl, 2004 .

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 .

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 .

Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data

Melissa B. Rivers, Ralf Rudnik, Jürgen Quest, 2015 .

High Reynolds number transition experiments in ETW (TELFONA project)

Stefan Hein, Uwe Fey, Raffaele Donelli, 2010 .

ETW: simulations of true flight behaviour

Jürgen Quest, 2001 .

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 .

Investigation of a Pressure-Sensitive Paint Technique for ETW

Ulrich Henne, Christian Klein, Jürgen Quest, 2017 .

INVESTIGATION OF A MODERN TRANSONIC TRANSPORT AIRCRAFT CONFIGURATION OVER A LARGE RANGE OF REYNOLDS NUMBERS

Jürgen Quest, Airbus Uk, Stephen Rolston, 2002 .

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

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

High-Reynolds Number Aeroacoustic Testing Under Pressurised Cryogenic Conditions in PETW

Thomas Ahlefeldt, Jürgen Quest, J. Quest, 2012 .

Development of New Two-Component TSP for Cryogenic Testing

Uwe Fey, Jürgen Quest, Yasuhiro Egami, 2007 .

Progress in Optical Measurement Methods in Cryogenic Conditions

Ulrich Henne, Jürgen Quest, Robert Konrath, 2013 .

On Application of Surface Measurement Techniques for Cryogenic High Reynolds Number Investigations on Wind Tunnel Models

Wolfgang Nitsche, Jürgen Quest, Janin Leuckert, 2008 .

Development of new two-component temperature-sensitive paint (TSP) for cryogenic testing

Christian Klein, Uwe Fey, Jürgen Quest, 2012 .