FLOWCID · Flow Control for Industrial Design
Horizon 2020 — Marie Skłodowska-Curie Actions
- Duration
- 2021-08-01 → 2024-07-31
- EU contribution
- €263,732
- Participants
- 2
- Scheme
- MSCA-IF
Lines connect the coordinator with its partners.
Results in brief
Flow Control for Industrial Design
FLOWCID (Flow Control for Industrial Design) was a Marie Skłodowska-Curie Global Individual Fellowships funded by the Research Executive Agency (REA) under MSCA-IF-GF As part of the FLOWCID project, Prof. Eusebio Valero from the Universidad Politécnica de Madrid (Spain) spent 2 years at Purdue University (USA), collaborating with Prof. Guillermo Paniagua in the Zucrow Lab (https://engineering.purdue.edu/Zucrow), where he conducted a training and research programme. He then completed an additional year in the return phase, transferring the knowledge gained back to UPM. The main objective of FLOWCID was to develop new methods and tools for controlling flow unsteadiness, particularly the complex non-linear interactions observed in highly detached configurations and unstarting phenomena. To achieve this, FLOWICD proposed combining accurate (high-order) numerical simulations, flow stability and data analysis techniques, along with detailed experimental studies. This approach aimed to model the flow physics involved in Rotating Detonation Engines (RDEs), assess the sensitivity to perturbations, and ultimately define an actuator methodology for controlling these phenomena. To conclude, this action has provided the fellow with the opportunity to create strong links with American research groups, expand their network of contacts, learn about the educational system of American universities, and improve their knowledge in Fluid Mechanics and experimental facilities. Additionally, the fellow has gained a better understanding of the links between numerical and experimental simulations, facilitating knowledge transfer to and from UPM. Technically, improvements have been made in the state of the art in numerical simulation, particularly in the use of high-order schemes and their challenges in shock capturing, detached flows, and boundary layer interaction. The interpretation of experimental results, their uncertainties, and comparison with numerical results remain challenging. The creation of an advanced library for feature detection, which merges numerical and experimental data, has improved the accuracy and interpretation of results. Furthermore, new avenues for flow control have been explored, with initial designs indicating that much work remains, especially in unsteady, compressible, and highly detached flows. The project has had a positive impact on the fellow’s career, who is now internationally recognized in the field of numerical simulation, stability analysis, and flow control.
Data: CORDIS, © European Union
Project objective
Aviation contributes to more than 2% of global greenhouse gas (GHG) emissions, in the absence of further measures, carbon dioxide (CO2) emissions from international aviation are estimated to almost quadruple by 2050 compared to 2010. Efforts to reduce GHG through the development of alternatives to traditional fossil-fuelled thermal engines have made great strides. Yet large capacity, long-range electric vehicles with operating speeds similar to or faster than current commercial vehicles are not expected to become feasible for several decades due to the limitations of battery energy density and cost. An alternative short-term solution that is being investigated in Purdue University by Prof. Paniagua with intense interest worldwide is to utilize a rotating deto-nation engines (RDE) to improve the efficiency and reduce the size/weight of current thermal gas turbines. If utilized with hydrogen, with high energy-to-mass ratio and robust detonation properties, RDE will provide the best chance to realize long-range, high-payload flight with zero greenhouse gas emissions . However, the development and performance of a high-efficiency RDE is inhibited by two main fluid dynamic problems: the flow separation caused by high pressure gradients, and the unstarting phenomena across the internal turbine pas-sages. The numerical solution, analytical analysis and control of those problems is the main objective of FLOWCID.FLOWCID proposes a 24-month long outgoing phase (and 12 months return phase) of Prof. Eusebio Valero (the Researcher) from Universidad Politécnica de Madrid UPM (the Beneficiary), to Zucrow Labs, at Purdue University, USA (the Host) under the supervision of Prof. Guillermo Paniagua (the Supervisor).
Original text from CORDIS.
Participants
- UNIVERSIDAD POLITECNICA DE MADRID · MadridCoordinatorSpain
- TRUSTEES OF PURDUE UNIVERSITY · West LafayetteUnited States
Links
Data: CORDIS, © European Union
