CORDIS oferuje możliwość skorzystania z odnośników do publicznie dostępnych publikacji i rezultatów projektów realizowanych w ramach programów ramowych HORYZONT.
Odnośniki do rezultatów i publikacji związanych z poszczególnymi projektami 7PR, a także odnośniki do niektórych konkretnych kategorii wyników, takich jak zbiory danych i oprogramowanie, są dynamicznie pobierane z systemu OpenAIRE .
Rezultaty
Deliverable will define the main parameters of the cracking reactor; develop a concept of the cracking reactor design, assess its weight and overall dimensions; develop strapping, power supply and protection systems, mechanization of start-stop feeding of raw materials, removal and storage of reaction products.
Design of schemes for supplying energy to HTEP (odnośnik otworzy się w nowym oknie)Deliverable will develop a number of layouts to power the HTEP and evaluate the advantages and disadvantages of these layouts.
Comparative analysis and justification of the choice of on-board liquid hydrogen storage and supply systems. (odnośnik otworzy się w nowym oknie)Comparison of alternative locations. Volumes and shapes of LH tanks: option of replacing complete LH empty by full tanks, to avoid LH refuelling near gateways
Intermediate report on the results from the experimentation (odnośnik otworzy się w nowym oknie)This report describes the experimental result obtained from the first campaign conducted on the liquefaction, storage and vaporization test rig. This report refers to Task 3.4.
Specifications for Advisory Board (odnośnik otworzy się w nowym oknie)This document will describe the expected contribution of the Advisory Board, such as the revision of documents, participation in meetings, etc. It will be discussed in the Kick off meeting.
Further design modifications and newly reengineered (odnośnik otworzy się w nowym oknie)This will be mainly from Task 2.2.1. More thoroughly optimized GDL designs and tabulated macro-properties will be sought and reported after considering more design and aviation operational factors, such as clamping force and water-rich operations. Factors on channel flow regimes, which will be mainly discussed in Task 2.2.2, will also be briefly considered in Task 2.2.1 and reflected in this deliverable.
Shaping the GTE concept, selection of parameters and design scheme. Determination of GTE mass. Shaping the propeller concept, selection of parameters and design scheme. Determination of propeller mass (odnośnik otworzy się w nowym oknie)Deliverable will identify the parameters of the main engine components, the basic geometric parameters of the air-gas duct, the engine design diagram, developed a mathematical model of the engine, the choice of control laws and determined parameters in the main design points, selected design diagram of the engine, the evaluation of its mass and overall dimensions.Deliverable will also define the parameters of the propeller; the basic geometric parameters of the propeller; the method of controlling the propeller; the design scheme of the propeller, the evaluation of its mass and overall dimensions.
Requirements for HTEP elements (odnośnik otworzy się w nowym oknie)Deliverable will identify critical mass and size requirements (for all elements), required power and fuel consumption for the gas turbine engine, electric engine power and efficiency, required propeller parameters, and required FC performance parameters for HTEP elements.
Analysis of the Liquid hydrogen system for aero engine applications (odnośnik otworzy się w nowym oknie)The report describes the technical results of the process simulation of the systems comprising liquid hydrogen tank, cryogenic pump, and vaporizer for use in both gas turbines and fuel cells, which differ, among others, in the pressurization level. The results include also the main technical specification for the main equipment listed above. This deliverable refers to Task 3.1.
Report on the realization of the liquefaction, storage and vaporization test rig and on the update of the combustion test rig (odnośnik otworzy się w nowym oknie)This report describes the design criteria and the design work of the liquefaction, storage and vaporization test rig. Moreover, it describes the construction procedure, focusing on the issues encountered and the solutions adopted. This report refers to Task 3.3.
Report the promising technologies to reduce aviation noise exposure at airports around the EU and world (odnośnik otworzy się w nowym oknie)The currently investigated promising technologies (EU Clean Sky and Clean Aviation programs, USA FAA and NASA programs CLEEN and ASCENT) will be evaluated.
Planning and report on the dissemination and outreach activities (odnośnik otworzy się w nowym oknie)Update of D11.1. Reporting and assessment of communication and dissemination activities carried out. (i) 1st version: M18; (ii) updated 2nd version: M36; (iii) updated 3rd version: M48
Results of aircraft emission inventory estimation for current fleet and projected trends of aviation neutrality by 2050 (odnośnik otworzy się w nowym oknie)Assessment of aircraft contribution to global emission for current fleet and updated fleet for the CAEP/EUROCONTROL mid-and long-term forecasting scenarios will be delivered. Inventory assessment will be provided for the classes of aircraft
Shaping the cracking case concept, determination of its mass. Shaping the EE concept, determination of its mass (odnośnik otworzy się w nowym oknie)Deliverable will develop the concept of the evaporator, taking into account the possible design and layout, the type of hot coolant; investigate the features of the hydrogen boiling process using experimental data and CFD modeling; determine the design of the evaporator and its mass and dimensions.
Review of existing proposals in the field of creating hybrid turbo-electric propulsions for regional aircraft using fuel cells (odnośnik otworzy się w nowym oknie)Review and analysis of existing and currently developed hybrid propulsion systems for aviation applications, including fuel cells (FC). Technical problems of their production and operation. Advantages and disadvantages of existing and currently developed hybrid propulsion systems.
Prospects for (i) emissions free aviation, (ii) local air quality, and (iii) airport noise (odnośnik otworzy się w nowym oknie)This deliverable will assess the impact on NOx and other emissions, on local air quality, and on noise at airports of the introduction of new technologies in each class of aircraft as soon as they are mature up to 2050. It will be a combined outcome of tasks 10.1, 10.2 and 10.3.
Results of aircraft noise assessment at aircraft, airport and fleet levels with complementarily analysis of their calculation and measuring tools (odnośnik otworzy się w nowym oknie)Assessment of aircraft noise exposure at airport level for current fleet and updated fleet for the CAEP/EUROCONTROL mid-and long-term forecasting scenarios will be delivered. Noise exposure assessment will be realised by calculations at airport level due to change in aircraft design and fleet transformation till 2050.
Types and roles of battery powered aircraft (odnośnik otworzy się w nowym oknie)This deliverable will analyse relevant technologies in detail, bearing in mind that they may be different for distinct classes of aircraft. It will also address other issues, gaps or risks factors precluding the proper and timely development and implementation of the market of electrical small short range aircrafts powered by batteries. It will be the outcome of task 6.2 Batteries production and disposal sustainable life cycle
The concept of a hydrogen-fuelled combustion chamber. (odnośnik otworzy się w nowym oknie)Development of combustion chamber design concept for LH. Compatibility with burning fossil fuels and sustainable aviation fuels (SAFs).
Results of emission inventory estimation for updated fleet via selected technologies for the different classes of aircraft (odnośnik otworzy się w nowym oknie)Assessment of aircraft contribution to global emission for current fleet and updated fleet via selected technologies for the CAEP/EUROCONTROL mid-and long-term forecasting scenarios will be delivered. Inventory assessment will be provided for the classes of aircraft.
Exploitation and IPR management Plan and reporting activities (odnośnik otworzy się w nowym oknie)Description of the overall exploitation strategy and follow-up activities reporting of the consortium and the actions to be carried out by each partner. Detailed outline of the actions until the end of the project and in the 2 years following the project’s end.Description of the guidelines for Intellectual Property Rights (IPR) management as derived from the EFACA Grant Agreement and Consortium Agreement. A procedure is presented covering identification of potential innovations, documentation, tracking and protection of Intellectual Property derived from the EFACA project.(i) 1st report: M6; (ii) 2nd report: M18; (iii) 3rd report: M36; (iv) 4th report: M48
Results of aircraft noise assessment at aircraft, airport and fleet levels for updated fleet via selected technologies for the different classes of aircraft (odnośnik otworzy się w nowym oknie)Assessment of aircraft noise local exposure for current fleet and updated fleet via selected technologies for the CAEP/EUROCONTROL mid-and long-term forecasting scenarios will be delivered. Noise exposure assessment will be realised by calculations at airport level due to disruptive change in aircraft design and novel fleet transformation till 2050.
Report the promising technologies to reduce global aviation emission (odnośnik otworzy się w nowym oknie)The currently investigated promising technologies for fuel burn and engine emission reduction (EU Clean Sky and Clean Aviation programs, USA FAA and NASA programs CLEEN and ASCENT) will be evaluated
Management and Coordination Handbook (odnośnik otworzy się w nowym oknie)This document will guide and support the management and implementation of EFACA, deploying all the relevantinformation and tools for this purpose.
Elaboration of requirements for the main components of the HTEP: GTE, FC, EE, propeller (odnośnik otworzy się w nowym oknie)Deliverable will define the final concept of an advanced fuel cell for HTEP, identify the challenges in further building the HTEP, and generate requirements for its components
Report on gap analysis to achieve ACARE 2050 emission goals by comparison emission inventory results current fleet and updated fleet via selected technologies (odnośnik otworzy się w nowym oknie)Gap analysis in fuel/energy consumption and emission inventory assessment for the classes of aircraft at LTO and cruise levels will be performed. Gap analysis will be provided for the classes of aircraft.
Application of battery technologies to aircraft (odnośnik otworzy się w nowym oknie)This deliverable will study the current state, as well as the potential and limitations of the battery power for small short-range aircraft including UAM. It will be the outcome of task 6.1 Advances in battery technology
Technical and economic indicators of the systems. (odnośnik otworzy się w nowym oknie)Technical specifications and associated operating procedures and costs of acquisition and maintenance.
Preliminary shaping of the concept and typical flight profile of the aircraft with HTEP. Preliminary requirements for HTEP (odnośnik otworzy się w nowym oknie)Deliverable will tentatively conceptualize the aircraft, taking into account HTEP with fuel cells, forming preliminary requirements for HTEP with respect to safety issues and its operation when flying from sea level to cruising altitude
Shaping the FC concept of hydrocarbon fuel – electrical energy (odnośnik otworzy się w nowym oknie)Deliverable will define the basic parameters of FC, develop the FC design concept with an estimate of its mass and overall dimensions; form the conditions for FC placement in the aircraft design, taking into account the hydrogen feed scheme.
Advances on SAF properties and compatibility (odnośnik otworzy się w nowym oknie)Report on the existing and new technologies of production of SAF as it concerns possible raw materials, complexity of the technological process and its readiness level. Moreover, the compatibility of SAF with existing today aircraft systems and infrastructures will be considered (Task 9.2).
Rationale for the choice of design solutions in the development of liquid hydrogen in aircraft fuel systems. (odnośnik otworzy się w nowym oknie)Components of the liquid hydrogen system from storage tank to combustion chamber. Available technologies to meet cryogenic requirements of the liquid hydrogen.
Shaping the FC concept of hydrogen – electrical energy (odnośnik otworzy się w nowym oknie)Deliverable will define the basic parameters of FC, develop a FC design concept with an estimate of its mass and overall dimensions; form the conditions for FC placement in the aircraft design, taking into account the hydrogen feed scheme.
Calculation of the aircraft characteristics with various variants of the HTEP as for a typical flight profile (odnośnik otworzy się w nowym oknie)Deliverable will provide recommendations for further optimization of the aircraft-HTEP system based on the analysis of aircraft performance obtained with different energy supply schemes.
Shaping the vaporizer concept, determination of its mass (odnośnik otworzy się w nowym oknie)Deliverable will develop the concept of the evaporator, taking into account the possible design and layout, the type of hot coolant; investigate the features of the hydrogen boiling process using experimental data and CFD modeling; determine the design of the evaporator and its mass and dimensions.
Report on hydrogen-fired propulsion (odnośnik otworzy się w nowym oknie)The report describes the process simulation of pure-hydrogen fired gas turbines, touching also on the expected issues of flame stability and NOx formation. This deliverable refers to Task 3.2.
Refinement of the aircraft concept based on the adopted HTEP scheme. Clarification of requirements for HTEP (odnośnik otworzy się w nowym oknie)Deliverable will define the final concept for a regional aircraft with up to 80 seats and a range of 1,000 km with fuel cell for HTEP
Data Management Plan (odnośnik otworzy się w nowym oknie)A DMP describes the data management life cycle for the data to be collected, processed and/or generated by EFACA project. Detailed information on the procedures that will be implemented by the EFACA complying with national and EU legislation will be provided.(i) 1st report: M6; (ii) 2nd report: M18; (iii) 3rd report: M36; (iv) 4th report: M48
Selection of the optimal scheme for providing energy to HTEP (odnośnik otworzy się w nowym oknie)Deliverable will determine the optimal scheme for HTEP energy supply with FC based on the research conducted in Task 7.3. and in accordance with the evaluation criteria selected in Task 7.1.2.
Report on gap analysis to achieve ACARE 2050 aircraft noise goals by comparison the results for current and updated aircraft fleets via selected technologies (odnośnik otworzy się w nowym oknie)Gap analysis in aircraft noise reduction at source and exposure assessment for the classes of aircraft at LTO will be performed. Gap analysis will be provided for the classes of aircraft.
Communication and Dissemination Plan (odnośnik otworzy się w nowym oknie)Definition of how, when and where to communicate the project’s activities and results to a wide range of target groups. Will include the general communication activities (common to the whole consortium) and the contribution of all partners, as each partner will complete a table with their planned dissemination events and their possibilities of “spreading the word” about the project. Communication materials: Project logo and identity, leaflet, poster, roll-up, templates will be developed.
Concepts of hydrogen-fuelled engine fuel system. (odnośnik otworzy się w nowym oknie)Development of the LH fuel system concept, including theoretical study of structural schemes of the LH fuel system.
Design of components of liquid hydrogen fuel system. (odnośnik otworzy się w nowym oknie)Installation of LH tanks and system components in the chosen aircraft configuration; effects on aerodynamics, structure, weight, performance, stability and control.
Current pathways for SAF production (odnośnik otworzy się w nowym oknie)Description of the situation in Europe and worldwide about the production of SAF with emphasis on the new pathways approval and the perspectives on the emerging techniques (Task 9.1).
Selection of criteria for evaluating HTEP schemes (odnośnik otworzy się w nowym oknie)Deliverable will review existing comprehensive criteria for evaluating the effectiveness of a propulsion system as part of an aircraft. New criteria for evaluating HTEP efficiency are selected or proposed, with environmental friendliness in mind.
Recommendations to the project, safety instructions and environmental safety when using hydrogen. (odnośnik otworzy się w nowym oknie)Operating aspects of liquid hydrogen including volatility, flammability, venting, modes of operation and safety.
Feasibility study report for the aircraft. (odnośnik otworzy się w nowym oknie)Design and comparison of two LH fuelled aircraft configurations: (i) a conventional tube and wing with LH tanks in AFT fuselage behind rear pressure bulkhead or in under fuselage cargo hold: (ii) a novel flying wing with LH tanks distributed in fuselage and wing.
The deliverable will describe, obtained technical characteristics of the developed EE, after tests on the test bench of FED company for their compliance with the specification from IVCHENKO: for example, power and efficiency of the motor, range of working frequencies of the output shaft, torque, dimensions and weight. There will be a description of the developed EE control system.
Publikacje
Autorzy:
Jan Friedrich Hellmuth, Philipp Rainer Menke, Arne Graf von Schweinitz, Patrick Koschel, Wilhelm Tegethoff, Michael Heere, Christiane Thomas, Jürgen Köhler
Opublikowane w:
Applied Thermal Engineering, Numer 280, 2026, ISSN 1359-4311
Wydawca:
Elsevier BV
DOI:
10.1016/J.APPLTHERMALENG.2025.127275
Autorzy:
K.Kazhan, K. Synylo, O. Zaporozhets S. Karpenko
Opublikowane w:
International Journal Sustainable Aviation, 2023
Wydawca:
N/A
DOI:
10.1504/IJSA.2023.127489
Autorzy:
Vitalii Makarenko, Vadim Tokarev, Kateryna Kazhan, Kateryna Synylo, Olexandr Yakushenko, Oleksandr Zaporozhets
Opublikowane w:
International Journal of Sustainable Aviation, ISSN 0000-0000
Wydawca:
Inderscience Publishers
DOI:
10.1504/IJSA.2024.142562
Autorzy:
Kateryna Kazhan
Opublikowane w:
Transactions on Aerospace Research, ISSN 0000-0000
Wydawca:
Łukasiewicz Research Network – Institute of Aviation in Warsaw.
DOI:
10.2478/TAR-2025-0003
Autorzy:
O. Zaporozhets M. Katsman V. Matsiuk ZAPOROZHETS, O.; KATSMAN, M.; MATSIUK, V.; MYRONENKO, V.
Opublikowane w:
Reliability: Theory & Applications, ISSN 0000-0000
Wydawca:
Reliability Theory Applications
DOI:
10.24412/1932-2321-2024-278-576-593
Autorzy:
Musab Hammas Khan, Patrizia Lamberti, Vincenzo Tucci
Opublikowane w:
Inorganics, Numer 13, 2025, ISSN 2304-6740
Wydawca:
MDPI AG
DOI:
10.3390/INORGANICS13020062
Autorzy:
Boichenko S., Danilin O., Shkilniuk I., Yakovlieva A., Khotian A., Pavlovskyi M., Lysak Roksolana, Shamanskyi S., Kriuchkov A., Tarasiuk O.
Opublikowane w:
Eastern-European Journal of Enterprise Technologies, 2023
Wydawca:
N/A
DOI:
10.15587/1729-4061.2023.280046
Autorzy:
Synylo K.,Makarenko V., Krupko A., Tokarev V
Opublikowane w:
Eastern-European Journal of Enterprise Technologies, 2024
Wydawca:
N/A
DOI:
10.15587/1729-4061.2024.302793
Autorzy:
Horobtsov, I., Cherniak, L., Radomska, M., Tykhenko, O., & Synylo, K.
Opublikowane w:
Ecological Safety and Balanced Use of Resources Journal, 2023
Wydawca:
N/A
DOI:
10.31471/2415-3184-2023-14(2)-09
Autorzy:
Oleksandr Zaporozhets, Vitalii Makarenko, Vadim Tokarev, Kateryna Kazhan, Kateryna Synylo
Opublikowane w:
Sustainable Aviation, The Future of Electric Aviation and Artificial Intelligence, 2024
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-62094-2_23
Autorzy:
Renata Adami, Patrizia Lamberti, Maria Sarno, Vincenzo Tucci
Opublikowane w:
Sustainable Aviation, The Future of Electric Aviation and Artificial Intelligence, 2024
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-62094-2_11
Autorzy:
Rosa Maria Arnaldo Valdés, Victor Fernando Gómez Comendador, Maria Zamarreño Suarez, Francisco Perez Moreno, Raquel Delgado-Aguilera Jurado
Opublikowane w:
Sustainable Aviation, The Future of Electric Aviation and Artificial Intelligence, 2024
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-62094-2_12
Autorzy:
Kateryna Kazhan, Vitalii Makarenko, Vadym Tokarev, Kateryna Synylo, Oleksander Zaporozhets, Andrzej Chyla, Michal Bukala
Opublikowane w:
Sustainable Aviation, The Future of Electric Aviation and Artificial Intelligence, 2024
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-62094-2_19
Autorzy:
K. Synylo, O. Zaporozhets, A. Krupko, K. Kazhan, V. Makarenko, V. Tokarev, S. Karpenko
Opublikowane w:
Sustainable Aviation, The Future of Electric Aviation and Artificial Intelligence, 2024
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-62094-2_18
Autorzy:
A. Chyla, M. Bukala, K. Kazhan, V. Makarenko, V. Tokarev, O. Zaporozhets
Wydawca:
MDPI
DOI:
10.1007/978-3-031-62094-2_25
Autorzy:
Abdullah Bamoshmoosh, Gianluca Valenti
Opublikowane w:
Sustainable Aviation, The Future of Electric Aviation and Artificial Intelligence, 2024
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-62094-2_16
Autorzy:
K.Synylo, A.Krupko,V. Makarenko, O. Zaporozhets
Opublikowane w:
"Book of abstracts of X International Scientific-Technical Conference ""THEORY AND PRACTICE OF RATIONAL USE OF TRADITIONAL AND ALTERNATIVE FUELS AND LUBRICANTS"""
Wydawca:
Scientific edition
Autorzy:
V. Makarenko, O.Yakushenko, V.Tokarev, K.Kazhan, K. Synylo, O. Zaporozhets
Opublikowane w:
"Book of abstracts of X International Scientific-Technical Conference ""THEORY AND PRACTICE OF RATIONAL USE OF TRADITIONAL AND ALTERNATIVE FUELS AND LUBRICANTS"""
Wydawca:
Springer Nature
DOI:
10.1007/978
Autorzy:
Oleksandr Zaporozhets, Vitalii Makarenko, Vadim Tokarev, Kateryna Kazhan
Opublikowane w:
Lecture Notes in Networks and Systems, Advances in Civil Aviation Systems Development, 2025
Wydawca:
Springer Nature Switzerland
DOI:
10.1007/978-3-031-91992-3_13
Autorzy:
Musab Hammas Khan, Patrizia Lamberti, Vincenzo Tucci
Opublikowane w:
2025 IEEE International Conference on Environment and Electrical Engineering and 2025 IEEE Industrial and Commercial Power Systems Europe (EEEIC / I&CPS Europe), 2025
Wydawca:
IEEE
DOI:
10.1109/EEEIC/ICPSEUROPE64998.2025.11169152
Autorzy:
K.Synylo, V.Makarenko, A.Krupko,O.Zaporozhets,O.Yakushenko, V.Tokarev
Opublikowane w:
2025
Wydawca:
EUCASS
Autorzy:
Yurii Ulitenko, Maksym Kirichkov, Igor Kravchenko
Wydawca:
Proceedings of the EUCASS 2025
DOI:
10.13009/EUCASS2025-409
Autorzy:
Kazhan К.І., Makarenko V.M, Tokarev V.I.
Opublikowane w:
Proceedings of ІІ International Scientific and Methodical Conference “Protection of the population, territories and critical infrastructure objects – education, science, practice”, Kyiv, May 22 – 23, 2025
Wydawca:
І International Scientific and Methodical Conference “Protection of the population, territories and critical infrastructure objects – education, science, practice
Autorzy:
Francesca Iapaolo and Fabio Cozzi
Opublikowane w:
Journal of Physics: Conference Series
Wydawca:
IOP Publishing
DOI:
10.1088/1742-6596/3063/1/012007
Autorzy:
Rosa Maria Arnaldo Valdés*, Victor Fernando Gómez Comendador, Maria Zamarreño, Suarez, Francisco Perez Moreno, and Raquel Delgado-Aguilera Jurado
Opublikowane w:
International Symposium on Electric Aircraft and Autonomous Systems, 2024, ISSN 0000-0000
Wydawca:
IOP SCIENCE
DOI:
10.1088/1742-6596/2716/1/012012
Autorzy:
T. Hikmet KARAKOÇ Oleksandr ZAPOROZHETS Andrzej LESKI Ali Haydar ERCAN Alper DALKIRAN
Opublikowane w:
International Symposium on Electric Aircraft and Autonomous Systems, 2023, ISSN 0000-0000
Wydawca:
N/A
Autorzy:
Oleksandr Zaporozhets
Opublikowane w:
IST25-66
Wydawca:
MDPI
Autorzy:
T. Hikmet Karakoc, Oleksandr Zaporozhets, Alper Dalkiran, Ali Haydar Ercan
Opublikowane w:
Proceedings of the 2023 International Symposium on Electric Aviation & Autonomous Systems and the International Symposium on Unmanned Systems, AI, Design & Efficiency
Wydawca:
Springer
DOI:
10.1007/978-3-031-62094-2
Autorzy:
Francesca Iapaolo and Fabio Cozzi
Opublikowane w:
Journal of Physics: Conference Series
Wydawca:
IOP Publishing
DOI:
10.1088/1742-6596/3063/1/012007
Autorzy:
Sergiy Dmytriyev and Andrii Yedynovych, Oleksandr Korniichuk, Oleksandr Kolokolov, Igor Kravchenko
Opublikowane w:
Proceedings of the EUCASS 2025
Wydawca:
EUCASS
Autorzy:
Rosa Maria Arnaldo Valdés, Maria Zamarreño Suarez , Francisco Perez Moreno, Raquel Delgado-Aguilera Jurado,Victor Fernnado Gómez Comendador
Opublikowane w:
Proceeding of EUCASS-2025
Wydawca:
EUCASS
DOI:
10.13009/EUCASS2025-401
Autorzy:
Serhii Fil , Dmytro Berbenets , Andrii Khaustov , Oleksandra Urban, Oleksandr Bondarchuk
Wydawca:
MDPI
Autorzy:
Musab Hammas Khan, Vincenzo Tucci, Patrizia Lamberti, Raffaele Longo, Liberata Guadagno
Opublikowane w:
EASN 2024, 2025
Wydawca:
MDPI
DOI:
10.3390/ENGPROC2025090039
Autorzy:
María ZAMARREÑO SUÁREZ, Rosa María ARNALDO VALDÉS, Francisco PÉREZ MORENO, Raquel DELGADO-AGUILERA JURADO and Víctor Fernando GÓMEZ COMENDADOR
Opublikowane w:
Proceeding of EUCASS-2025
Wydawca:
EUCASS
DOI:
10.13009/EUCASS2025-400
Autorzy:
Oleksandr ZAPOROZHETS, Kateryna KAZHAN, Vadim TOKAREV, Vitalii MAKARENKO, Andrzej CHYLA
Opublikowane w:
2025
Wydawca:
TSAS 2025 proceeding
DOI:
10.60711/TSAS25.20250217.7202472767080516
Autorzy:
Serhii Fil , Dmytro Berbenets , Andrii Khaustov , Oleksandra Urban, Oleksandr Bondarchuk
Opublikowane w:
Proceeding of EUCASS-2025
Wydawca:
EUCASS
Autorzy:
María Zamarreño Suárez,Francisco Pérez Moreno,Raquel Delgado-Aguilera Jurado,César Gómez Arnaldo and Víctor Fernando Gómez Comendador
Opublikowane w:
Engineering Proceedings
Wydawca:
MDPI
DOI:
10.3390/ENGPROC2025090037
Autorzy:
Fabio Cozzi, Francesca Iapaolo, Edoardo Ciuffoli and Pierfelice Rocco
Opublikowane w:
Proceeding of EUCASS-2025
Wydawca:
EUCASS
DOI:
10.13009/EUCASS2025-404
Autorzy:
Sergii Fil, Dmytro Berbenets, Khaustov Andrii, Urban Oleksandra and Bondarchuk Oleksandr
Opublikowane w:
International Symposium on Electric Aircraft and Autonomous Systems (ISEAS-23), 2023, ISSN 0000-0000
Wydawca:
N/A
Autorzy:
K. Kazhan, V.Makarenko, A. Chyla, O.Zaporozhets, V.Tokarev
Opublikowane w:
Proceeding of EUCASS-2025
Wydawca:
EUCASS
DOI:
10.13009/EUCASS2025-406
Autorzy:
D. Terlizzi, A. Bamoshmoosh, G. Valenti
Opublikowane w:
9th European Congress on Computational Methods in Applied Sciences and Engineering, 2025
Wydawca:
CIMNE
DOI:
10.23967/ECCOMAS.2024.249
Autorzy:
Boichenko, Sergii Yakovlieva, Anna Zaporozhets Oleksandr
Opublikowane w:
2023, ISSN 0000-0000
Wydawca:
N/A
DOI:
10.1007/978-3-031-34350-6
Autorzy:
Ribun, V., Boichenko, S., Yakovlieva, A., Chelaydyn, L., Dubrovska, V., Shkyar, V., Wos, P.
Opublikowane w:
Systems, Decision and Control in Energy IV. Studies in Systems, Decision and Control, vol 454. Springer, Cham., 2023
Wydawca:
SPRINGER NATURE
DOI:
10.1007/978-3-031-22464-5_19
Autorzy:
Boichenko S., Zaporozhets A., Yakovlieva A., Shkilniuk I.
Opublikowane w:
Studies in Systems, Decision and Control, vol 510. Springer, Cham, 2024
Wydawca:
N/A
DOI:
10.1007/978-3-031-44351-0
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