Innovating Works
Mostrando 1 al 20 de 27 resultados
HEAVEN: Hydrogen Engine Architecture Virtually Engineered Novelly STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un HORIZON EUROPE: HORIZON-JU-Clean-Aviation-2022-01 Climate-neutral aviation will require the use of alternative fuels such as Green Hydrogen and Sustainable Aviation Fuel (SAF) combined with...
2022-12-09 - 2026-12-31 | Financiado
UP Wing: Ultra Performance Wing STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un HORIZON EUROPE: HORIZON-JU-Clean-Aviation-2022-01 The Ultra Performance Wing project will validate, down select, mature and demonstrate key technologies and provide the architectural integra...
2022-12-08 - 2026-06-30 | Financiado
DISPROP: Aerodynamic and aeroacoustic modeling of closely operating propellers for DIStributed PROPulsion STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP11-2020-01 DISPROP aims at improving the current aerodynamic and aeroacoustic analysis and design capabilities for large aircraft operating with distri...
2020-12-11 - 2023-10-31 | Financiado
RHEA: Robust and sustainable by design ultra higH aspEct ratio wing and Airframe STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP10-2019-01 The efficiency gains offered by ultra-high aspect ratio wings are key to increase the sustainability of air travel as the volume of passenge...
2020-04-15 - 2023-11-30 | Financiado
ALVAR: Advance Laminar Flow Control with Variable Porosity STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP10-2019-01 Laminar Flow Control by means of a suction system appears to be one of the most promising technologies to significantly reduce the pollutant...
2020-03-30 - 2022-05-31 | Financiado
NIFTI: Non Intrusive Flow distortion measurements within a Turbofan Intake STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un H2020: H2020-CS2-CFP09-2018-02 Short and slim aero-engine intake designs for very high bypass ratio configurations cause notable levels of unsteady distortions at the fan...
2019-10-01 - 2023-10-31 | Financiado
IVANHOE: Installed adVAnced Nacelle uHbr Optimisation and Evaluation STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP09-2018-02 The introduction of UHBR engines poses new challenges on optimal nacelle design, both in geometry and in location. In response to the topic...
2019-09-26 - 2023-10-31 | Financiado
ATTILA: Advanced Testbed for TILtrotor Aeroelastics STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP09-2018-02 The ATTILA project is aimed at the design, manufacture and testing of an advanced testbed for aeroelastic wind tunnel testing of tiltrotor a...
2019-09-20 - 2023-12-31 | Financiado
ESTRO: Experimental and theoretical aSsessmenT of laminaR flow rObusteness at high mach and reynolds number... STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP08-2018-01 According to the requirements of the topic JTI-CS2-2018-CFP08-REG-03-01, the proposal ESTRO will produce experimental and numerical data in...
2019-03-05 - 2022-12-31 | Financiado
TRINIDAT: Tilt Rotor INlet Innovative Design And Testing STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP08-2018-01 The TRINIDAT project adresses the aerodynamic characterization of an already available intake geometry (as supplied by ITD) and optimization...
2019-02-26 - 2022-04-30 | Financiado
UHURA: Unsteady High Lift Aerodynamics Unsteady RANS Validation STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-MG-2016-2017 UHURA aims at validating unsteady numerical simulations of the aerodynamics of high-lift systems during deployment and retraction. In detail...
2018-05-17 - 2022-08-31 | Financiado
NEXTTRIP: NEXT generation civil Tilt Rotor Interactional aerodynamic tail oPtimisation STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-CS2-CFP06-2017-01 The aerodynamic configuration definition of the NGCTR needs to be confirmed by a large scale powered wind tunnel experiment, with the aim to...
2018-02-14 - 2020-08-31 | Financiado
RINGO: Research Infrastructures Needs Gaps and Overlaps STICHTING DUITSNEDERLANDSE WINDTUNNELS participó en un H2020: H2020-EE-2016-2017 RINGO will deliver a holistic identification of research infrastructure needs, gaps and overlaps for the aviation sector in Europe with resp...
2017-02-02 - 2020-02-29 | Financiado
L-CROR CTS: Low speed aerodynamic test of large CROR aircraft model in a closed test section STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un FP7: "Tests will be performed on a full model with installed CROR engines. The model will be mounted on a ventral sting, located at tunnel centre...
Financiado
PLAAT: Aeroacoustic and aerodynamic wind tunnel tests at low speed for a turbofan model equipped with TPS STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un FP7: "The noise shielding empennage designs for rear fuselage mounted engines are promising enough to further investigate. Significant noise redu...
Financiado
LAc-LORR OTS: Low speed aeroacoustic test of an open rotor powered complete model STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un FP7: Tests will be performed on a full model provided with installed Counter Rotating Open Rotor (CROR) engines. The 1:7 scale model, provided by...
Financiado
BLAME: Breakthrough Laminar Aircraft Model wind tunnel testing in Europe STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un FP7: "Natural laminar flow wings will be flight tested, within a project called BLADE. A new outer laminar wing will be fitted on the legacy A340...
Financiado
L-CROR OTS: Low speed aeroacoustic test of large aircraftmodel with open rotor engines STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un FP7: "Tests will be performed on full model with installed CROR engines. The model will be mounted on a dorsal sting, located at tunnel centre li...
Financiado
LAAME-CROW: Advanced Measurement Techniques in a Low Speed CROR Wind Tunnel Test STICHTING DUITSNEDERLANDSE WINDTUNNELS tramitó un FP7: "Tests will be performed on a full model provided with installed Counter Rotating Open Rotor (CROR) engines. The 1:7 scale model, provided b...
Financiado
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