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Opendata, web and dolomites

PRODIGE SIGNED

PRediction of aerOdynamics and hinge moment loaDs at hIgh mach and fliGht rEynolds number

Total Cost €

EC-Contrib. €

Partnership

Views

Outcomes and
results

PRODIGE project word cloud

Explore the words cloud of the PRODIGE project. It provides you a very rough idea of what is the project "PRODIGE" about.

parallel room elastic instrumentation review campaign inside angles parts experimental manufactured successively simplified validated suitably modify accurate assembled prototype connection aileron moment ailerons close deflection jig calibration modified perform experiments setup data measuring reynolds premises deformation wing manager vtcr equipped matrix floor 16 according experimentally hinge business critical chamber efficiency performed static jet transonic mock model manufacture first suitable sent cryogenic final surface validation prodige tested prediction mach wind tunnel flight loads balance etw surfaces climate

Project "PRODIGE" data sheet

The following table provides information about the project.

Coordinator	IBK-INNOVATION GMBH & CO. KG Organization address address: BUTENDEICHSWEG 2 city: HAMBURG postcode: 21129 website: www.ibk-innovation.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	Germany [DE]
Project website	https://www.ibk-innovation.de/prodige
Total cost	2˙211˙276 €
EC max contribution	2˙211˙276 € (100%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP06-2017-01
Funding Scheme	CS2-RIA
Starting year	2018
Duration (year-month-day)	from 2018-03-01 to 2020-08-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	IBK-INNOVATION GMBH & CO. KG IBK-INNOVATION GMBH & CO. KG Organization address address: BUTENDEICHSWEG 2 city: HAMBURG postcode: 21129 website: www.ibk-innovation.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (HAMBURG)	coordinator	1˙337˙360.00
2	DEHARDE GMBH DEHARDE GMBH Organization address address: AM HAFEN 14A city: VAREL postcode: 26316 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (VAREL)	participant	590˙910.00
3	DREAM INNOVATION SRL DREAM INNOVATION SRL Organization address address: VIA F. PARRI 1 city: SANT'ARPINO postcode: 81030 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (SANT'ARPINO)	participant	161˙053.00
4	TECHNISCHE UNIVERSITAT DARMSTADT TECHNISCHE UNIVERSITAT DARMSTADT Organization address address: KAROLINENPLATZ 5 city: DARMSTADT postcode: 64289 website: www.tu-darmstadt.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (DARMSTADT)	participant	121˙951.00

Map

Project objective

According to the requirements of the topic, the proposal PRODIGE will produce experimentally accurate loads and hinge moment data at high Mach and flight Reynolds numbers. The data will be the result of an experimental test campaign performed in the European Transonic Wind (ETW) tunnel; as a result they will be available for other future programmes to improve the loads and efficiency prediction of control surfaces. At this aim, the consortium PRODIGE has, first of all, to perform the design of the experimental setup. This means to design/ modify and manufacture all the required parts of an existing 1/16 scale model of a business jet according to technical requirements provided by the Topic Manager. In parallel, the consortium PRODIGE will design and manufacture a prototype hinge moment balance for the ailerons of the wind tunnel model including all the instrumentation necessary for the experiments. This hinge moment balance will be tested for calibration and validation in the cryogenic climate room VTCR by using a simplified mock-up and a suitable jig for loads application and for providing a connection to the chamber floor. The mock-up will be equipped with the aileron of the model or a similar control surface suitably modified to allow applying calibration loads. The validated design of the hinge moment balance concept will be then implemented in the final design of the wind tunnel model. A critical design review will close the design phase. Successively the model parts will be manufactured and the model assembled and sent to ETW premises where it will be tested against static loads in the climate room (VTCR) for measuring the elastic deformation of the wing, and then finally tested at several Reynolds and Mach numbers (flight conditions) and at several aileron deflection angles (the test matrix will be defined in agreement with the topic Manager) inside ETW.

Deliverables

List of deliverables.
Data Management Plan (DMP)	Open Research Data Pilot	2019-11-20 16:04:35
Project Progress Report	Documents, reports	2019-11-20 16:04:35
Dissemination & Exploitation Plan	Documents, reports	2019-11-20 16:04:35

Take a look to the deliverables list in detail: detailed list of PRODIGE deliverables.

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The information about "PRODIGE" are provided by the European Opendata Portal: CORDIS opendata.