CADENCE DESIGN SYSTEMS BELGIUM
- Country
- Belgium
- Type
- Beneficiary
- Website
- www.numeca.com
- Grants received
- 36
Funding record
- 36 grants on record
- €9,593,636.88 awarded in total
- 2007–2025 span of the record
Grants recorded here are the ones our sources publish, and the total is the sum of those. It is not a statement of this organisation's total funding.
Programmes
14 further grants are on record without a programme named by the source, or under a programme outside the largest shown here.
Frequent partners
Organisations this one has been funded alongside on two or more projects. A single shared consortium is not counted: the largest here has 195 members, and being on one list together is not a collaboration.
- DEUTSCHES ZENTRUM FUR LUFT - UND RAUMFAHRT EV
- CENTRE INTERNACIONAL DE METODES NUMERICS EN ENGINYERIA
- VON KARMAN INSTITUTE FOR FLUID DYNAMICS
- INSTITUT NATIONAL DE RECHERCHE EN INFORMATIQUE ET AUTOMATIQUE
- IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE
- UNIVERSIDAD POLITECNICA DE MADRID
- STICHTING KONINKLIJK NEDERLANDS LUCHT - EN RUIMTEVAARTCENTRUM
- AIRBUS DEFENCE AND SPACE GMBH
Calls from this organisation
No published calls from this organisation.
Grants received
- Advanced CMOS Technology for 10 A node
- 14 Anstrom CMOS IC technology
- Stability and Sensitivity Methods for Flow Control and Industrial Design
- Advanced Modeling CapabiLities For UHBR Low Noise Fan Technology
- Multi-Site Coupled Simulation for Advanced collaborative design
- Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications
- Advanced Steady and unsTeady distORtion sImulAtor
- HIGH-FIDELITY LES/DNS DATA FOR INNOVATIVE TURBULENCE MODELS
- Advanced High-Order Simulation Methods for Industrial Applications
- Industrial decision-making on complex production technologies supported by simulation-based engineering
- Innovative Methodologies and technologies for reducing Aircraft noise Generation and Emission
- Stability and Sensitivity Methods for Industrial Design
- An Exascale Programming, Multi-objective Optimisation and Resilience Management Environment Based on Nested Recursive Parallelism
- Aeroelastic Gust Modelling
- Towards Industrial LES/DNS in Aeronautics – Paving the Way for Future Accurate CFD
Data source
© European Union, 2026. Source: CORDIS. Reused under Commission Decision 2011/833/EU — CC BY 4.0.
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