Conference & Journal Papers

A culture of continous improvements is part of ETW's DNA. Adaptability and agility from self-reflection and learning is valued as a key to our success. Publications given on or closely related to ETW are one performance indicator in this respect, and are listed here sorted by date, recent first.

TITLE OF PAPER AUTHOR(S) PUBLICATION DATE, PLACE
Aeroacoustic testing on a full aircraft model at high Reynolds numbers in the European Transonic Windtunnel T. Ahlefeldt, D. Ernst, A. Goudarzi, H.-G. Raumer, C. Spehr, DLR Journal of Sound and Vibration 566 December 2023
First Comparison of CFD Simulation and Wind Tunnel Test of the Forward-Swept Natural Laminar Flow Model NLF-ECOWING-FSW S. Helm, K. Davies, M. Fehrs, DLR New Results in Numerical and Experimental Fluid Mechanics XIV September2023
CFD-basierte Transitionsvorhersage für den Entwurf von Laminarflugzeugen S. Helm, DLR Deutscher Luft- und Raumfahrtkongress 2023 September 2023
Temperature Sensitive Paint measurement in ETW for investigation of the natural laminar flow on an innovative forward swept wing N.P. van Hinsberg, U. Henne, A. Weiss, S. Risius, C. Klein, DLR Deutscher Luft- und Raumfahrtkongress 2023 September 2023
Untersuchung der Umsetzbarkeit eines aeroelastisch ähnlichen Halbmodells für den Europäischen transsonischen Windkanal (ETW) T. Klimmek, DLR Deutscher Luft- und Raumfahrtkongress 2023 September 2023
Entwicklung eines laseroptischen Punktsensors auf Basis der Filtered Rayleigh Scattering Technik zum Einsatz unter kryogenen Bedingungen A.-K. Hensch, P. Guntermann, ETW
M. Dues, G. Stockhausen, DLR
30. Fachtagung "Experimentelle Strömungsmechanik" der GALA e.V. September 2023
Contribution of Scientific Computing in European Research and Innovation for Greening Aviation D. Knoerzer, Independent Aeronautics Consultant, Brussels Impact of Scientific Computing on Science and Society. Computational Methods in Applied Science 58 July 2023
Contribution to the 7th AIAA CFD Drag Prediction Workshop Using TAS-code and FaSTAR A. Sansica, M. Murayama, Y. Ito, A. Hashimoto, JAXA
R. Furuya, Ryoyu Systems Co., Ltd
AIAA AVIATION 2023 Forum
AIAA 2023-3397
June 2023, San Diego, CA, USA
Mach and Reynolds number effects on transonic buffet on the XRF-1 transport aircraft wing at flight Reynolds number A. Waldmann, M. C. Ehrle, J. Kleinert, Uni Stuttgart
D. Yorita, DLR
T. Lutz, Uni Stuttgart
Experiments in Fluids 64 May 2023
Prediction of wing buffet pressure loads using a convolutional and recurrent neural network framework R. Zahn, A. Weiner, C. Breitsamter, TU München CEAS Aeronautical Journal March 2023
Time-resolved pressure-sensitive paint measurements for cryogenic wind tunnel tests D. Yorita, U. Henne, C. Klein, DLR CEAS Aeronautical Journal January 2023
Temperature-Sensitive Paint measurements in combination with Carbon-Fiber-Reinforced Plastic models in cryogenic conditions C. Klein, J. Lemarechal, U. Henne, S. Koch, DLR
V. Ondrus, FH Münster
A.-K. Hensch, ETW
Sven Schaber, Airbus
AIAA SciTech 2023 Forum
AIAA 2023-1460
January 2023, National Harbor, MD, USA
Remote control actuated wind tunnel models: design and testing best practices F. T. Calkins, D. Nicholson, M. Carpenter, A. Lafranchi, Boeing
D. R. Saxer, C. Cramer, NASA
AIAA SciTech 2023 Forum
AIAA 2023-1459
January 2023, National Harbor, MD, USA
Embedded WMLES of transonic buffet on a nacelle-aircraft configuration M. Herr, TU Braunschweig
S. Spinner, A. Probst, DLR
R. Radespiel, TU Braunschweig
R. Rudnik, DLR
AIAA SciTech 2023 Forum
AIAA 2023-0246
January 2023, National Harbor, MD, USA
Characterization of Transonic Buffet on a Swept Wing by Means of Cryogenic PIV C.J. Schauerte, J. Bosbach, R. Konrath, R. Geisler, DLR
F. Philipp, A.-M. Schreyer, RWTH Aachen
Deutscher Luft- und Raumfahrtkongress 2022 September 2022,
January 2023
Experimental Assessment of Wing Lower Side Buffet Effects Induced by the Installation of a UHBR Nacelle S. Spinner, R. Rudnik, DLR CEAS Aeronautical Journal December 2022
Research Initiative for Numerical and Experimental Studies on High Speed Stall of Civil Aircraft T. Lutz, J. Kleinert, A. Waldmann, Uni Stuttgart
L. Koop, D. Yorita, DLR
G. Dietz, M. Schulz, ETW
Journal of Aircraft 60 (3) November 2022
Prediction of transonic wing buffet pressure based on deep learning R. Zahn, C. Breitsamter, TU München CEAS Aeronautical Journal November 2022
Recent Activities on Flow Quality Assessment at the European Transonic Windtunnel J.H. You, M.C.N. Wright, H. Quix, ETW ICAS 2022, 33rd International Congress of the Aeronautical Sciences September 2022
Stockholm, Sweden
The UK National Wind Tunnel Facility L. Doherty, University of Oxford
C. Mc Namara, K. Gouder, J. Morrison, Imperial College
2nd International Conference on High-Speed Vehicle Science and Technology September 2022
Bruges, Belgium
A new Efficient Method for Transition Detection with TSP by use of Infra-Red Laser Heating A.-K. Hensch, P. Guntermann, ETW 8th Japanese-German Joint Seminar on Molecular Imaging Technology for Interdisciplinary Research
Oral Presentation
September 2022, Virtual Event
A New Balance for New Testing Capabilities - ETW's New Balance B010 and the Lean Secondary Roll Mechanism H. Quix, ETW 12th International Symposium on Strain-Gauge Balances
Oral Presentation
May 2022, Buffalo, NY, USA
Half-Span Model Testing Capability at the European Transonic Windtunnel (ETW) J.H. You, ETW 12th International Symposium on Strain-Gauge Balances
Oral Presentation
May 2022, Buffalo, NY, USA
Limited Utility of Self-made Oxygen Generators Assembled From Everyday Commodities During the COVID-19 Pandemic U. Limper, L. Klaas, M. Köhler, D. Lichte, DLR
N. Maldonado Samaniego, USFQ
J. Suarez, JHU
J. Jordan, B. Hoffschmidt, DLR
Disaster Medicine and Public Health Preparedness 1-4 May 2022
Model Mounting K. Hufnagel, TU Darmstadt Wind Tunnel Balances, Experimental Fluid Mechanics, Springer April 2022
Investigation of Pressure and Temperature Sensitive Paint Measurements under Background Lights and Deformation D.Yorita, U. Henne, C. Klein, DLR AIAA SciTech 2022 Forum
AIAA 2022-1940
January 2022, San Diego, CA, USA
Time resolved pressure measurements by means of PSP in cryogenic conditions C. Klein, DLR AIAA SciTech 2022 Forum
AIAA 2022-1938
January 2022, San Diego, CA, USA
Enhancing Capabilities - ETW's New Lean Secondary Roll Mechanism (LSRM) H. Quix, ETW AIAA SciTech 2022 Forum
Invited Oral Presentation
January 2022, San Diego, CA, USA
Development of the Remotely Controlled Aileron Actuator (RCAA) for High Reynolds Number Testing at ETW H. Quix, ETW AIAA SciTech 2022 Forum
Invited Oral Presentation
January 2022, San Diego, CA, USA
National Research Initiative for Numerical and Experimental Studies on High-Speed Stall Phenomena of Civil Aircraft T. Lutz, J. Kleinert, A. Waldmann, Uni Stuttgart Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.3 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
Pressure Sensitive Paint Measurement In ETW For Investigation Of Unsteady Flow And Interaction Phenomenon D. Yorita, U. Henne, C. Klein, DLR Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.3 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
Design of a UHBR Through Flow Nacelle for High-Speed Stall Wind Tunnel Investigations S. Spinner, R. Rudnik, DLR Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.3 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
Numerical Simulation of Wake Tail Plane Interactions on a Tandem Wing Configuration in High-Speed Stall Conditions J. Kleinert, T. Lutz, M. Blind, A. Beck, Uni Stuttgart Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.3 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
Prediction of Transonic Wing Buffet Pressures Based on Neural Network Approaches R. Zahn, C. Breitsamter, TU München Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.4 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
flowTorch - A platform for analysis and reduced-order modeling of high speed stall flow phenomena A. Weiner, R. Semaan, TU Braunschweig Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.4 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
Wall-Modeled Large-Eddy Simulation of Ramp Flow Separation with the Discontinuous Galerkin Framework FLEXI M. Blind, T. Kuhn, A. Beck, Uni Stuttgart Deutscher Luft- und Raumfahrtkongress 2021
Session Q2.4 DFG/HGF High Speed Stall Research Initiative
September 2021, Virtual Event
Principles of Model Deformation Measurements at ETW H. Quix, ETW AIAA Aviation 2021 Forum
Oral Presentation
August 2021, Virtual Event
Comparison of Heating Methods for Transition Detection by TSP on a Generic Nacelle in the Pilot ETW P. Guntermann, ETW Aerospace Europe Conference 2020
Presentation 128
February 2020, Bordeaux, France
Unsteady Pressure Measurements by means of PSP in Cryogenic Conditions C. Klein, D. Yorita, U. Henne, T. Kleindienst, S. Koch, DLR
V. Ondrus, FH Münster
58th AIAA Aerospace Sciences Meeting
AIAA 2020-0122
January 2020, Orlando, FL, USA
Application of Temperature Sensitive Paint to Investigate Laminar-to-Turbulent Transition on Nacelles C. Klein, D. Yorita, U. Henne, DLR
V. Ondrus, FH Münster
A.-K. Hensch, R. Longo, A. Gimbel, ETW
S. von Deetzen, Deharde
58th AIAA Aerospace Sciences Meeting
AIAA 2020-1608
January 2020, Orlando, FL, USA
A New Efficient Method for Transition Detection by TSP on a Full Span Model by use of Infra-Red Laser A.-K. Hensch, ETW 58th AIAA Aerospace Sciences Meeting
Oral Presentation
January 2020, Orlando, FL, USA
Progress on Shape Memory Alloy Remote Control Actuation (SMARCA) Testing in Cryogenic Facilities F.T. Calkins, D.E. Nicholson, M.A. Sleppy, M.S. Carpenter, A.F. Lafranchi, Boeing,
S. von Deetzen, M. Müller, C. Clark, Deharde
M.C.N. Wright, H. Quix, A.-K. Hensch, ETW
D.R. Saxer, C.J. Cramer, NASA
58th AIAA Aerospace Sciences Meeting
Oral Presentation
January 2020, Orlando, FL, USA
Low & High Speed Cryogenic Testing of a Wind Tunnel Model With Remote Control Actuation (RCA) Spoiler F.T. Calkins, M.S. Carpenter, A.F. Lafranchi, D.E. Nicholson, M.A. Sleppy, Boeing,
R.C. Griffiths, AeroTEC,
S. von Deetzen, M. Müller, Deharde
M.C.N. Wright, ETW
C.J. Cramer, D.R. Saxer, NASA
AIAA Aviation 2019 Forum
AIAA 2019-2975
June 2019, Dallas, TX, USA
Shape Memory Alloy enabled Remote Control Actuated High Speed Cryogenic Wind Tunnel Models D.E. Nicholson, F.T. Calkins, M.A. Sleppy, M.S. Carpenter, A.F. Lafranchi, Boeing,
S. von Deetzen, M. Müller, Deharde
M.C.N. Wright, H. Quix, A.-K. Hensch, ETW
D.R. Saxer, C.J. Cramer, NASA
SMST (Shape Memory and Superelastic Technologies) Conference May 2019
Comparison of microphone array measurements in the closed test section of LSWT and ETW C. Spehr, T. Ahlefeldt, DLR CEAS Aeronautical Journal 10 (1) March 2019
Investigation of Hybrid Laminar Flow Control (HLFC) on a 2D-Model in the Cryogenic Pilot European Transonic Windtunnel (PETW) A.-K. Hensch, P. Guntermann, R. Longo, J. Quest, P. Okfen, ETW
C. Klein, S. Risius, DLR
S. Schaber, Airbus
57th AIAA Aerospace Sciences Meeting
AIAA 2019-1181
January 2019, San Diego, CA, USA
Boundary layer transition detection on wind tunnel models during continuous pitch traverse C. Klein, D. Yorita, U. Henne, DLR
V. Ondrus, U. Beifuss, Uni Hohenheim
A.-K. Hensch, R. Longo, ETW
57th AIAA Aerospace Sciences Meeting
AIAA 2019-1180
January 2019, San Diego, CA, USA
New Verification Concept for ETW’s 25 kN Balance Calibration Machine J.H. You, H. Quix, J. Semmelmann, T. Baumgart, F.-J. Ernst, W. Strudthoff, ETW 11th International Symposium on Strain-Gauge Balances May 2018, Cologne, Germany
Lattice Boltzmann Simulation of the ETW Slotted Wall Test Section B. König, E. Fares, EXA
M. Wright, ETW
NATO STO Symposium AVT-284, 12-1 - 12-14 April 2018, Turin, Italy
ESWIRP: European Strategic Wind tunnels Improved Research Potential program overview G. Boyet, ONERA CEAS Aeronautical Journal 9 (2) February 2018
Using wing model deformation for improvement of CFD results of ESWIRP project P. Vrchota, A. Prachař, VZLU CEAS Aeronautical Journal 9 (2) February 2018
Summary of the 2012 Boeing 787 Half Span Model High Speed Test at the European Transonic Windtunnel (Invited) M.A. Sleppy, Boeing 56th AIAA Aerospace Sciences Meeting
AIAA 2018-1137
January 2018, Kissimmee, FL, USA
Successful Application of Cryogenic Pressure Sensitive Paint Technique at ETW D. Yorita, C. Klein, U. Henne, DLR
V. Ondrus, U. Beifuss, Uni Hohenheim
A.-K. Hensch, R. Longo, P. Guntermann, J. Quest, ETW
56th AIAA Aerospace Sciences Meeting
AIAA 2018-1136
January 2018, Kissimmee, FL, USA
Wind-Tunnel and CFD Investigations Focused on Transition and Performance Predictions of Laminar Wings D. Hue, O. Vermeersch, J. Duchemin, ONERA
O. Colin, D. Tran, Dassault Aviation
AIAA Journal 56 (1) January 2018
High-speed PIV applied to wake of NASA CRM model at high Re-number sub- and transonic stall conditions R. Konrath, R. Geisler, J. Agocs, H. Ehlers, F. Philipp, DLR
J. Quest, ETW
CEAS Aeronautical Journal 9 (2) August 2017
Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data M. Rivers, NASA
J. Quest, ETW
R. Rudnik, DLR
CEAS Aeronautical Journal 9 (2) July 2017
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 9 (2) 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 flow structures in the near-field wake region of the Common Research Model D.-M. Zimmermann, A. Waldmann, T. Lutz, E. Krämer, Uni Stuttgart CEAS Aeronautical Journal 9 (2) December 2016
Unsteady Wake of the NASA Common Research Model in Low-Speed Stall A. Waldmann, P.P. Gansel, T. Lutz, E. Krämer, Uni Stuttgart Journal of Aircraft 53 (4) July 2016
Assessment and validation of aerodynamic performance results for a Natural Laminar Flow transonic wing tested in cryogenic conditions via simulation of turbulent wedges in CFD A. Styles, Airbus
S. Risius, DLR
RAeS 2016 Applied Aerodynamics Conference 19-21 July 2016
Prediction and Measurement of the Common Research Model Wake at Stall Conditions T. Lutz, P.P. Gansel, A. Waldmann, D.-M. Zimmermann, S. Schulte am Hülse, Uni Stuttgart Journal of Aircraft 53 (2) March 2016
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
Validation of Wing Deformation Simulations for the NASA CRM Model using Fluid-Structure Interaction Computations S. Keye, R. Rudnik, DLR 53rd AIAA Aerospace Sciences Meeting
AIAA 2015-0619
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
ICAS 2003, 23rd International Congress of Aeronautical Sciences – 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
The European Transonic Wind Tunnel: ETW High Quality Performance With High Productivity J. A. Tizard, X. Bouis, ETW Interntl. Gas Turbine and Aeroengine Congress and Exposition June 1994,
The Hague, Netherlands
Status of the European Transonic Windtunnel (ETW) X. Bouis, ETW Deutscher Luft- und Raumfahrtkongress 1993
Session Windkanal-Technologie (Kryo-Technik)
September 1993,
Göttingen, Germany