Conference & Journal Papers

This section contains publications given on ETW, sorted by date, recent first.

TITLE OF PAPER AUTHOR(S) PUBLICATION DATE, PLACE
A numerical approach for assessing slotted wall interference using the CRM model at ETW I.A. Kursakov, A.R. Gorbushin, S.M. Bosnyakov, S.A. Glazkov, A.V. Lysenkov, S.V. Matyash, A.V. Semenov, TsAGI
J. Quest, ETW
CEAS Aeronautical Journal 8 June 2017
Microphone Array Measurement in European Transonic Wind Tunnel at Flight Reynolds Numbers Thomas Ahlefeldt, DLR AIAA Journal 55 (1) January 2017
Application of Carbon Nanotubes and Temperature- Sensitive Paint for the Detection of Boundary Layer Transition under Cryogenic Conditions C. Klein, U. Henne, D. Yorita, DLR
U. Beifuss, V. Ondrus, Uni Hohenheim
A.-K. Hensch, R. Longo, M. Hauser, P. Guntermann, J. Quest, ETW
55th AIAA Aerospace Sciences Meeting
AIAA 2017-0336
January 2017, Grapevine, TX, USA
Investigation of a Pressure-Sensitive Paint Technique for ETW D. Yorita, C. Klein, U. Henne, DLR
V. Ondrus, U. Beifuss, Uni Hohenheim
A.-K. Hensch, P. Guntermann, J. Quest, ETW
55th AIAA Aerospace Sciences Meeting
AIAA 2017-0335
January 2017, Grapevine, TX, USA
Development of a Highly Sensitive Temperature-Sensitive Paint for Measurements under Cryogenic Temperature (100K–160K) Conditions C. Klein, U. Henne, M. Costantini, DLR
V. Ondrus, U. Beifuss, Uni Hohenheim
J. Zhai, DNW
J. Quest, ETW
54th AIAA Aerospace Sciences Meeting
AIAA 2016-0650
January 2016, San Diego, CA, USA
Application of Lifetime-based Pressure-Sensitive Paint Technique to Cryogenic Wind Tunnel Tests D. Yorita, C. Klein, U. Henne, DLR
V. Ondrus, U. Beifuss, Uni Hohenheim
A.-K. Hensch, P. Guntermann, J. Quest, ETW
54th AIAA Aerospace Sciences Meeting
AIAA 2016-0649
January 2016, San Diego, CA, USA
Design, Manufacture and Commissioning of a new NLR Half Model Balance for ETW M. Wright, ETW
B.R. Nahuis, B.A.T. Noordman, W.J. Vankan, NLR
53rd AIAA Aerospace Sciences Meeting
AIAA 2015-1788
January 2015, Kissimmee, FL, USA
Flight Test Tailored ETW Testing of a Commercial Transport High Lift Configuration R. Rudnik, N. Bier, DLR
J. Quest, M. Schulz, ETW
53rd AIAA Aerospace Sciences Meeting
AIAA 2015-1559
January 2015, Kissimmee, FL, USA
Dynamic Measurements on the NASA CRM Model tested in ETW H. Quix, A-K Hensch, ETW 53rd AIAA Aerospace Sciences Meeting
AIAA 2015-1097
January 2015, Kissimmee, FL, USA
High-Speed PIV Applied to Wake of NASA CRM Model in ETW Under High Re-Number Stall Conditions for Sub- and Transonic Speeds R. Konrath, R. Geisler, J. Agocs, D. Otter, H. Ehlers, F. Philipp, DLR
J. Quest, ETW
53rd AIAA Aerospace Sciences Meeting
AIAA 2015-1095
January 2015, Kissimmee, FL, USA
Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited) M. Rivers, NASA
J. Quest, ETW
R. Rudnik, DLR
53rd AIAA Aerospace Sciences Meeting
AIAA 2015-1093
January 2015, Kissimmee, FL, USA
Slotted Wall Interference Investigation in ETW using the NASA CRM model A.R. Gorbushin, S.M. Bosnyakov, S.A. Glazkov, I.A. Kursakov, A.V. Lysenkov, S.V. Matyash, A.V. Semenov, TsAGI
J. Quest, ETW
53rd AIAA Aerospace Sciences Meeting
AIAA 2015-0621
January 2015, Kissimmee, FL, USA
Modification of the Control & Measurement Software for the Balance Calibration Machine at ETW J. Mantik, H. Quix, W. Strudthoff, U. Jansen, and F.J. Ernst, ETW 9th Balance Calibration Symposium
Paper 18
May 2014
Assessing Model Dynamics within the Critical Alpha Range H. Quix, W. Strudthoff, ETW 52nd AIAA Aerospace Sciences Meeting
AIAA 2014-1484
January 2014, National Harbor, MD, USA
Real-Flight Microphone-Array Measurements on a Scaled Model in ETW T. Ahlefeldt, DLR
J. Quest, ETW
52nd AIAA Aerospace Sciences Meeting
AIAA 2014-1483
January 2014, National Harbor, MD, USA
Going for Experimental and Numerical Unsteady Wake Analyses Combined with Wall Interference Assessment by Using the NASA CRM Model in ETW T. Lutz, P. P. Gansel, Univ. Stuttgart
J.-L. Godard, ONERA
A. Gorbushin, TsAGI
R. Konrath, DLR
J. Quest, ETW
S.M.B. Rivers, NASA
51st AIAA Aerospace Sciences Meeting
AIAA 2013-0871
January 2013, Grapevine, TX, USA
Enhancement of the Stereo Pattern Tracking Technique for Model Deformation Assessment at ETW J. Mantik, H. Quix, J. Quest, ETW 51st AIAA Aerospace Sciences Meeting
AIAA 2013-0870
January 2013, Grapevine, TX, USA
Flow Field Measurements by PIV at High Reynolds Numbers R. Konrath, J. Agocs, R. Geisler, D. Otter, E.W.M. Roosenboom, T. Wolf, DLR
J. Quest, ETW
51st AIAA Aerospace Sciences Meeting
AIAA 2013-0869
January 2013, Grapevine, TX, USA
Development of new two-component temperature-sensitive paint (TSP) for cryogenic testing Y. Egami, AIT
U. Fey, C. Klein, DLR
J. Quest, ETW
V. Ondrus, U. Beifuss, Uni Hohenheim
Measurement Science and Technology 23 (11) October 2012
High-Reynolds Number Aeroacoustic Testing Under Pressurised Cryogenic Conditions in PETW T. Ahlefeldt, DLR
J. Quest, ETW
50th AIAA Aerospace Sciences Meeting
AIAA 2012-0107
January 2012, Nashville, TN, USA
HINVA - High lift INflight VAlidation - Project Overview and Status R. Rudnik, DLR
D. Reckzeh, Airbus
J. Quest, ETW
50th AIAA Aerospace Sciences Meeting
AIAA 2012-0106
January 2012, Nashville, TN, USA
Numerical Maximum Lift Predictions of a Realistic Commercial Aircraft in Landing Configuration N. Bier, D. Rohlmann, R. Rudnik, DLR 50th AIAA Aerospace Sciences Meeting
AIAA 2012-0279
January 2012, Nashville, TN, USA
Hotwires in Pressurized, Cryogenic Environment - It Works! H. Quix, J. Quest, ETW 50th AIAA Aerospace Sciences Meeting
AIAA 2012-0105
January 2012, Nashville, TN, USA
Problem of Interference of an Ogival Body of Revolution With the Wind-Tunnel Sting And Specific Features of Computing This Problem S. Bosnyakov, V. Vlasenko, I. Kursakov, S. Mikhaylov, TsAGI
J. Quest, ETW
TsAGI Sciences Journal 41 (2) 2011
A short history of the European Transonic Wind Tunnel ETW J. Green, ARA
J. Quest, ETW
Progress in Aerospace Sciences 47 (5) July 2011
Aero-Structural Wind Tunnel Experiments with Elastic Wing Models at High Reynolds Numbers (HIRENASD - ASDMAD) J. Ballmann, A. Boucke, B.-H. Chen, L. Reimer, M. Behr, A. Dafnis, C. Buxel, S. Buesing, H.-G. Reimerdes, K.-H. Brakhage, H. Olivier, RWTH Aachen University
M. Kordt, J. Brink-Spalink, F. Theurich, A. Büscher, Airbus
49th AIAA Aerospace Sciences Meeting
AIAA 2011-0882
January 2011, Orlando, FL, USA
Complementary Numerical and Experimental Data Analysis of the ETW Telfona Pathfinder Wing Transition Tests T. Streit, K.-H. Horstmann, DLR
G. Schrauf, Airbus
S. Hein, U. Fey, Y. Egami, DLR
J. Perraud, I. S. El Din, ONERA
U. Cella, Piaggio AI
J. Quest, ETW
49th AIAA Aerospace Sciences Meeting
AIAA 2011-0881
January 2011, Orlando, FL, USA
Hot-Wire Measurements in Cryogenic Environment H. Quix, J. Quest, C. Brzek, ETW 49th AIAA Aerospace Sciences Meeting
AIAA 2011-0880
January 2011, Orlando, FL, USA
Adaptation of PIV for Application in Cryogenic Pressurized Wind Tunnel Facilities at High Reynolds Numbers Robert Konrath, Dirk Otter, Reinhard Geisler, Janos Agocs, Hartmut Mattner, E.W.M. Roosenboom, Uwe Fey, DLR
Jürgen Quest, Christian Kühn, ETW
15th Int. Symp. on Applications of Laser Techniques to Fluid Mechanics
Paper 1572
July 2010
Transonic High Reynolds Number Transition Experiments in the ETW Cryogenic Wind Tunnel J. Perraud, ONERA
G. Schrauf, Airbus
I. Archambaud, ONERA
R. Donelli, CIRA
T. Streit, DLR
A. Hanifi, FOI
U. Fey, Y. Egami, S. Hein, DLR
J. Quest, ETW
48th AIAA Aerospace Sciences Meeting
AIAA 2010-1300
January 2010, Orlando, FL, USA
Advanced Measurement Techniques for High Reynolds Number Testing in Cryogenic Wind Tunnels U. Fey, R. Konrath, T. Kirmse, T. Ahlefeldt, J. Kompenhans, DLR 48th AIAA Aerospace Sciences Meeting
AIAA 2010-1301
January 2010, Orlando, FL, USA
Microphone-Array Measurements in a Cryogenic Wind Tunnel Thomas Ahlefeldt, Lars Koop, DLR AIAA Journal 48 (7) July 2010
Advanced Aeroelastic Testing at the German Aerospace Center (DLR) and Future Challenges H. Hönlinger, M. Böswald, H. Mai, DLR
G. Dietz, ETW
NATO RTO Symposium AVT-152, KNZ-1 - KNZ-31 May 2008, Loen, Norway
Computational Tools for Supporting the Testing of Civil Aircraft Configurations in Wind Tunnels S. Bosnyakov, I. Kursakov, A. Lysenkov, S. Matyash, S. Mikhailov, V. Vlasenko, TsAGI
J. Quest, ETW
Progress in Aerospace Sciences 44 (4), pp. 67 - 120, Elsevier Dec. 2007
Investigation of a Half-Model High-Lift Configuration in a Wind Tunnel P. Eliasson, FOI Sweden Journal of Aircraft 45 (1) Jan-Feb 2008
The FALCON 7X: from ETW to flight M. Stojanowski, E. Germain, Dassault Aviation 46th AIAA Aerospace Sciences Meeting
AIAA 2008-0835
January 2008
Reno, NV, USA
Stall Behaviour of the EUROLIFT High Lift Configurations R. Rudnik, DLR 46th AIAA Aerospace Sciences Meeting
AIAA 2008-0836
January 2008
Reno, NV, USA
Experimental Analysis of High Reynolds Number Aero-Structural Dynamics in ETW J. Ballmann et al., RWTH Aachen 46th AIAA Aerospace Sciences Meeting
AIAA 2008-0841
January 2008
Reno, NV, USA
On Application of Surface Measurement Techniques for Cryogenic High Reynolds Number Investigations on Wind Tunnel Models J. Leuckert, J. Domhardt, W. Nitsche, TU Berlin
J. Quest, ETW
46th AIAA Aerospace Sciences Meeting
AIAA 2008-0842
January 2008
Reno, NV, USA
Performance Testing with High Productivity in a Low Speed Flight Reynolds Number Test Campaign R.C. Griffiths, Boeing
M.C.N. Wright, ETW
ICAS 2006, 25th International. Congress of the Aeronautical Sciences September 2006
Hamburg, Germany
High Reynolds Number Aerostructural Dynamics Experiments in the ETW J. Ballmann, A. Dafnis, C. Braun, H. Korsch, H.-G. Reimerdes, H. Olivier, RWTH Aachen ICAS 2006, 25th International. Congress of the Aeronautical Sciences September 2006
Hamburg, Germany
New Generation of Cryogenic Wind Tunnel Models J. de Pablo Pérez, Airbus Spain,
M. Schulz, B. Hildebrand, ETW
EU, 5th Community Aeronautical Days June 2006
Vienna, Austria
Advanced Measurement Techniques at High Reynolds Number Testing in the ETW D. Schimanski, E. Germain, W. Strudthoff, ETW Aerospace Testing Expo 2005, Open Technology Forum April 2005
Hamburg, Germany
The M-DAW Project, Investigations in Novel Wing Tip Device Design A. Mann, Airbus UK
E. Elsholz, Airbus D
43rd AIAA Aerospace Sciences Meeting
AIAA-2005-0461
January 2005
Reno, NV, USA
Business Jet Type Configuration at ETW M. Stojanowski, Dassault-Aviation 43rd AIAA Aerospace Sciences Meeting
AIAA 2005-0460
January 2005
Reno, NV, USA
The Development and Application of Optical Measurement Techniques for High Reynolds NumberTesting in Cryogenic Environment E. Germain, J. Quest, ETW 43rd AIAA Aerospace Sciences Meeting
AIAA 2005-0458
January 2005
Reno, NV, USA
Numerical and Experimental Investigations of Slot Flow with Respect toWind Tunnel Wall Interference Assessment S.A. Glazkow, A.R. Gorbushin, A.I. Ivanow, A.V. Semenow, V.V. Vlasenko, TsAGI
J. Quest, ETW
42nd AIAA Aerospace Sciences Meeting
AIAA-2004-2308
January 2004
Reno, NV, USA
The ETW Wall Interference Assessment for Full and Half Models N. Gross, J. Quest, ETW 42nd AIAA Aerospace Sciences Meeting
AIAA 2004-0769
January 2004
Reno, NV, USA
On the Development of Planar Velocimetry Techniques for Cryogenic Wind Tunnels C. Willert, DLR
J. Quest, ETW
5th International Symposium on Particle Image Velocimetry September 2003
Busan, Korea
On the Development of Doppler Global Velocimetry for Cryogenic Wind Tunnels C. Willert, DLR,
J. Quest, U. Jansen, ETW
20th International Congress in Aerospace Simulation Facilities (ICIASF) August 2003,
Göttingen, Germany
Transition Detection by Temperature Sensitive Paint at Cryogenic Temperatures in the ETW U. Fey, DLR,
Y. Egami, NAL,
J. Quest, U. Jansen, ETW
20th International Congress in Aerospace Simulation Facilities (ICIASF) August 2003,
Göttingen, Germany
Model Deformation Measurement in ETW Using the Moiré Technique D. Pallek, K.A. Bütefisch, DLR
J. Quest, W. Strudthoff, ETW
20th International Congress in Aerospace Simulation Facilities (ICIASF) August 2003,
Göttingen, Germany
Tools and Techniques for high Reynolds Number Testing;
Status and Recent Improvements at ETW
D. Schimanski, J. Quest, ETW 41st AIAA Aerospace Sciences Meeting
AIAA 2003-0755
January 2003,
Reno, NV, USA
Testing of a Modern Transport Aircraft Configuration in ETW close to Mach = 0.9 S. Rolston, Airbus UK,
J. Quest, M.C. Wright, ETW
23rd International Congress of Aeronautical Sciences (ICAS) ICAS 2003 – 3.8.1 September 2002,
Toronto, Canada
ETW – A Facility for High Reynolds Number Testing G. Hefer, ETW IUTAM Symposium Transsonicum IV September 2002
Göttingen, Germany
First Measurements on an Airbus High Lift Configuration at ETW up to Flight Reynolds Numbers H. Hansen, EADS Airbus,
G.G. Mesuro, EADS-CASA
J. Quest, M.C. Wright, ETW
40th AIAA Aerospace Sciences Meeting
AIAA 2002-0423
January 2002,
Reno, NV, USA
Investigation of a Modern Transport Aircraft Configuration over a Large Range of Reynolds Numbers J. Quest, ETW,
S. Rolston, Airbus UK,
M.C. Wright, ETW
40th AIAA Aerospace Sciences Meeting
AIAA 2002-0422
January 2002,
Reno, NV, USA
ETW - Analytical Approach to Assess the Wing Twist of Pressure Plotted Wind Tunnel Models N. Gross, ETW 40th AIAA Aerospace Sciences Meeting
AIAA 2002-0310
January 2002
Reno, NV, USA
Development of the Half Model Testing Capability at ETW M.C. Wright, ETW DGLR-Fachtagung
“Messtechnik in kryogenen Windkanälen”
March 2001,
München, Germany
Der Europäische Transsonikwindkanal ETW – Mess- und Versuchstechnik in Gegenwart und Zukunft W. Burgsmüller, ETW DGLR-Fachtagung “Messtechnik in kryogenen Windkanälen” March 2001,
München, Germany
ETW - Simulations of True Flight Behaviour J. Quest, ETW EU Aeronautics Days No.3/4, Vol.3, Page 115 January 2001,
Hamburg, Germany
ETW – High Quality Test Performance in Cryogenic Environment J. Quest, ETW 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conf.
AIAA 2000-2206
June 2000,
Denver, CO, USA
The ETW, a Facility for High Reynolds Number Testing G. Hefer, D. Schimanski, ETW Interntl. Conference “New Technologies of Experimental Research and Simulation”, ILA 2000 June 2000,
Berlin, Germany