Explore the words cloud of the UHURA project. It provides you a very rough idea of what is the project "UHURA" about.
The following table provides information about the project.
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
|Coordinator Country||Germany [DE]|
|Total cost||6˙119˙233 €|
|EC max contribution||6˙119˙233 € (100%)|
1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
|Duration (year-month-day)||from 2018-09-01 to 2021-08-31|
Take a look of project's partnership.
|1||DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV||DE (KOELN)||coordinator||1˙646˙748.00|
|2||STICHTING DUITS-NEDERLANDSE WINDTUNNELS||NL (Marknesse)||participant||1˙072˙850.00|
|3||KUNGLIGA TEKNISKA HOEGSKOLAN||SE (STOCKHOLM)||participant||599˙750.00|
|4||IBK-INNOVATION GMBH & CO. KG||DE (HAMBURG)||participant||475˙000.00|
|5||OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES||FR (PALAISEAU)||participant||458˙062.00|
|6||STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM||NL (AMSTERDAM)||participant||385˙000.00|
|7||CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA||IT (CAPUA - CASERTA)||participant||331˙343.00|
|8||DASSAULT AVIATION||FR (PARIS)||participant||284˙915.00|
|9||INSTITUTO NACIONAL DE TECNICA AEROESPACIAL ESTEBAN TERRADAS||ES (TORREJON DE ARDOZ MADRID)||participant||237˙500.00|
|10||VYZKUMNY A ZKUSEBNI LETECKY USTAV AS||CZ (PRAHA 18)||participant||223˙125.00|
|11||ASCO INDUSTRIES N.V.||BE (ZAVENTEM)||participant||217˙438.00|
|12||AIRBUS OPERATIONS GMBH||DE (HAMBURG)||participant||187˙500.00|
UHURA aims at validating unsteady numerical simulations of the aerodynamics of high-lift systems during deployment and retraction. In detail we perform: - Validation of numerical simulation methods for prediction of the unsteady aerodynamics and dynamic loads during the deployment and retraction phase of high-lift systems. We expect to verify the ability of predicting the unsteady aerodynamics and corresponding loads on the Krueger flap within an accuracy comparable to steady state calculations (less than 1% error in lift, drag and pitching moment). - Quantification of the completely unknown aerodynamic characteristics of a slotted Krueger device during deployment and retraction. We expect to quantify the difference of the actual unsteady loads to the values obtained by state-of-the-art approaches to estimate the critical loads, which are either steady-state predictions or handbook estimations. And, we expect to achieve a system complexity reduction of about 70% by verifying the conceptual feasibility of a central drive architecture for a Krueger flap by properly assessing the handling qualities impact during the deployment. We also expect by this to keep the system weight at or below levels of current state-of-the-art slat devices. Further on, the higher accuracy for load calculations shall reduce the necessary safety margin for the structural sizing due to better knowledge of the actual loads. - Qualification of impact on handling qualities and certification. We expect the Research and Innovation Action to qualify the impact of the unsteady aerodynamic and of the dynamic loads during deployment on the handling qualities and certification issues. The latter also addresses the risk anand mitigation of failure cases.
|D51-4 Midterm Assessment Report||Documents, reports||2020-04-25 01:32:57|
|D52-1 Mid-term dissemination summary||Documents, reports||2020-04-25 01:33:08|
Take a look to the deliverables list in detail: detailed list of UHURA deliverables.
|year||authors and title||journal||last update|
Wallin S. (KTH), Hanifi, A. (KTH) and Bagheri, F. (neptech AB)
\"â€œUHURA Meshing Strategyâ€, part of \"\"Meshing and CFD strategies for large scale turboprop WT model integrating morphing high-lift devices\"\"\"
published pages: , ISSN: , DOI:
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