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 |
|---|---|---|---|
| Airbus, Pressure Measurements on the Transonic Aerofoil RAE2822 | M. Bouckley, P. White, J. Bonnefont, Airbus | National Wind Tunnel Facility, UK | August 2025 |
| Outlier Detection for Distributed Pressure Measurements | A. Barklage, L. Reimer, P. Bekemeyer, DLR | Journal of Aircraft 62 (AiA) | August 2025 |
| Development of NASA 2.7% Semispan and Full Span High Lift Common Research Models (CRM-HL) | M. Ertsgaard, C.S. Winski, NASA | AIAA AVIATION 2025 Forum AIAA 2025-3460 |
July 2025, Las Vegas, NV, USA |
| Validation of Natural Laminar Fin at Flight Reynolds Number | N. Tokugawa, T. Ishida, K. Ueshima, K. Ohira, JAXA | AIAA AVIATION 2025 Forum AIAA 2025-3289 |
July 2025, Las Vegas, NV, USA |
| Application of Temperature Sensitive Paint for High Altitude Transonic Natural Laminar Flow Design | T.R. Wayman, Otto Aviation J.G. Coder, Penn State N. Pfeiffer |
AIAA AVIATION 2025 Forum AIAA 2025-3185 |
July 2025, Las Vegas, NV, USA |
| Fusing CFD and measurement data using transfer learning | A. Barklage, P. Bekemeyer, DLR | arXiv:2507.20576 [cs.LG] | July 2025 |
| Transition prediction including turbulent wedges for a forward swept natural laminar flow wing | M. Fehrs, C. Kaiser, DLR | CEAS Aeronautical Journal 16 (3) | June 2025 |
| Scale Resolving Simulation of Buffet Effects Induced by Ultrahigh Bypass Ratio Nacelle Installation | S. Spinner, R. Rudnik, DLR M. Herr, TU Braunschweig A. Probst, DLR R. Radespiel, TU Braunschweig |
Journal of Aircraft 62 (3) | June 2025 |
| Deep Learning Framework for Predicting Transonic Wing Buffet Loads Due to Structural Eigenmode-Based Deformations | R. Zahn, M. Zieher, C. Breitsamter, TU München | Aerospace 2025 12(5) | May 2025 |
| Transonic High Reynolds Number Transition Model Validation Based on ETW Cryogenic Wind Tunnel Data | M. Fehrs, S. Helm, DLR | AIAA SciTech 2025 Forum Invited Paper AIAA 2025-1714 |
January 2025, Orlando, FL, USA |
| Aerodynamic Design of a Forward Swept NLF Wing for Short and Medium Range Aircraft | J.R. Bailo, DLR | AIAA SciTech 2025 Forum Invited Oral Presentation 4158666 |
January 2025, Orlando, FL, USA |
| Overview of the German LUFO Research Project ULTIMATE | H. Mai, DLR | AIAA SciTech 2025 Forum Invited Oral Presentation 4158665 |
January 2025, Orlando, FL, USA |
| Development of a Pitch Oscillator System for High Reynolds Number Testing at ETW | H. Quix, ETW | AIAA SciTech 2025 Forum Invited Oral Presentation 4158662 |
January 2025, Orlando, FL, USA |
| First Dynamic Test of a Laminar Wing at Realistic Flight Reynolds- and Mach-Numbers in the ETW | H. Mai, DLR | AIAA SciTech 2025 Forum Invited Oral Presentation 4158654 |
January 2025, Orlando, FL, USA |
| Demonstration of Natural Laminar Vertical Tail at High Reynolds Number Using a Cryogenic Wind Tunnel | N. Tokugawa, D. Kwak, T. Ishida, JAXA | AIAA SciTech 2025 Forum Invited Oral Presentation 4158633 |
January 2025, Orlando, FL, USA |
| News and Updates From the European Transonic Windtunnel | S. Gates, ETW | AIAA SciTech 2025 Forum Invited Oral Presentation 4158632 |
January 2025, Orlando, FL, USA |
| Development of Unsteady Measurement Techniques for High Reynolds Numbers at ETW | H. Quix, ETW | AIAA SciTech 2025 Forum Invited Oral Presentation 4158624 |
January 2025, Orlando, FL, USA |
| A CFD Validation Ecosystem to Advance the Prediction of Low-Speed Aerodynamics | J.P. Slotnik, Boeing | ICAS 2024, 34th International Congress of the Aeronautical Sciences | September 2024 Florence, Italy |
| Demonstration of natural laminar vertical tail at flight Reynolds number in ETW | N. Tokugawa, T. Ishida, JAXA, K. Ueshima, K. Ohira, Ryoyu Systems |
10th IUTAM Symposium on Laminar-Turbulent Transition Oral Presentation S8-3 |
September 2024 Nagano, Japan |
| Pressure based NLF design for vertical tail of conventional aircraft and wind tunnel test model | T. Ishida, JAXA, K. Ueshima, K. Ohira, Ryoyu Systems, N. Tokugawa, JAXA |
10th IUTAM Symposium on Laminar-Turbulent Transition Poster P26 |
September 2024 Nagano, Japan |
| Scale Resolving Simulation of Wing Lower Surface Buffet Effects Induced by the Installation of a UHBR Nacelle | S. Spinner, R. Rudnik, DLR M. Herr, TU Braunschweig A. Probst, DLR R. Radespiel, TU Braunschweig |
AIAA AVIATION 2024 Forum AIAA 2024-4264 |
July 2024, Las Vegas, NV, USA |
| Application of Temperature-Sensitive Paint for transition detection on an NLF forward-swept wing under harmonic pitch oscillation at flight-relevant Mach and Reynolds numbers | N.P. van Hinsberg, U. Henne, C. Klein, DLR | 21st International Symposium on Application of Laser and Imaging Techniques to Fluid Mechanics Oral Presentation |
July 2024 Lisbon, Portugal |
| Natural Laminar Flow at Cruise Mach Number 0.78: First Results of ETW Concept Verification Tests | A. Seitz, J.R. Bailo, T. Streit, DLR | ECCOMAS Congress 2024 | June 2024 Lisbon, Portugal |
| Comparison of Lifetime-Based Pressure-Sensitive Paint Measurements in a Wind Tunnel Using Model Pitch–Traverse and Pitch–Pause Modes | C. Klein, D. Yorita, U. Henne, DLR | Photonics 11 (6) | June 2024 |
| Numerical and experimental studies on high-speed stall phenomena | T. Lutz, A. Beck, Uni Stuttgart L. Koop, DLR |
CEAS Aeronautical Journal 15 (1) | March 2024 |
| Capturing Unsteady Flow Phenomena at High Speed Stall Conditions by Adaptation and Application of Cryogenic PIV | J. Bosbach, R. Konrath, R. Geisler, F. Philipp, J. Agocs, L. Koop, DLR C. Kühn, ETW |
AIAA SciTech 2024 Forum AIAA 2024-2665 |
January 2024, Orlando, FL, USA |
| Determination of the response time of TSP in cryogenic conditions | C. Klein, S. Risius, U. Henne, DLR V. Ondrus, FH Münster |
AIAA SciTech 2024 Forum AIAA 2024-1093 |
January 2024, Orlando, FL, USA |
| Investigation of Temperature Sensitive Paint Formulation for the Use from Cryogenic to Ambient Condition | D. Yorita, U. Henne, C. Klein, DLR V. Ondrus, FH Münster |
AIAA SciTech 2024 Forum AIAA 2024-1092 |
January 2024, Orlando, FL, USA |
| 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 | September 2023 |
| 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 15 (1) | March 2023 |
| Time-resolved pressure-sensitive paint measurements for cryogenic wind tunnel tests | D. Yorita, U. Henne, C. Klein, DLR | CEAS Aeronautical Journal 15 (1) | 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 15 (1) | 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 15 (1) | 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, EXAM.C.N. 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, AirbusS. 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.C.N. 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.N. 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.N. 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.N. 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.N. 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 |
