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CORDIS - Resultados de investigaciones de la UE
CORDIS

(LTO) noiSe and EmissioNs of supErsoniC Aircraft

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Emission estimations for the Ma 1.8 airliner (se abrirá en una nueva ventana)

In Task 4.2: Emission estimations for the Ma 1.8 airliner

Trajectory sensitivity study (se abrirá en una nueva ventana)

Results of trajectory sensitivity study shared by Task 5.5 with partners in WP5.

SST specific technologies: liner study (se abrirá en una nueva ventana)

Results of liner studies shared by Task 5.5 with partners in WP5.

Preliminary certification levels of Ma 1.8 airliner (se abrirá en una nueva ventana)

Report on noise certification level estimates for the preliminary status of the platform studied in T5.3 delivered to WP2, WP3 and WP6.

Assessment of emission climate impacts from stratospheric water and tropospheric and stratospheric ozone (se abrirá en una nueva ventana)

In Task 4.5: Assessment of emission climate impacts from stratospheric water and tropospheric and stratospheric ozone and linear contrails

Final certification levels of Ma 1.8 airliner (se abrirá en una nueva ventana)

Report on noise certification level estimates of the final Ma 1.8 airliner studied in T5.3 delivered to WP6.

Preliminary certification levels for Ma 2.2 airliner (se abrirá en una nueva ventana)

Report on noise certification level estimates for the preliminary status of the platform studied in T5.4 delivered to WP2, WP3 and WP6.

Key: CAEP 13 input (se abrirá en una nueva ventana)

Final report and presentation of project results available as CAEP 13 inputs – Dissemination of final SENECA results

Shielding study for Ma 2.2 airliner (se abrirá en una nueva ventana)

Results of shielding study for Ma 2.2 airliner delivered to partners in T5.4 for inclusion in the final noise certification estimates.

Initial sensitivity study on climate impact of supersonic aviation (se abrirá en una nueva ventana)

In Task 45 Initial sensitivity study on climate impact of supersonic aviation

Preliminary CAEP 13 input (se abrirá en una nueva ventana)

Draft Report and presentation of project results available for internal and advisory board review

SST specific technologies: shielding study (se abrirá en una nueva ventana)

Results of shielding study shared with by Task 5.5 with partners in WP5.

Final certification levels of Ma 2.2 airliner (se abrirá en una nueva ventana)

Report on noise certification level estimates of the final Ma 2.2 airliner studied in T5.4 delivered to WP6.

Emission estimations for the Ma 1.6 business jet aircraft (se abrirá en una nueva ventana)

In Task 4.2: Emission estimations for the Ma 1.6 business jet aircraft

SST noise technology assesement (se abrirá en una nueva ventana)

Report on noise related to SST specific technologies and its potential impact to EPNL certification levels delivered to WP6 by Task 5.5.

Shielding study Ma 1.8 airliner (se abrirá en una nueva ventana)

Results of shielding study delivered to partners in T5.3 for inclusion in the final noise certification estimates.

NASA STCA Noise assessment (se abrirá en una nueva ventana)

Report on NASA STCA PLR study and Noise assessment delivered to WP6 by Task 51

Final noise certification levels for Ma 1.6 business jet (se abrirá en una nueva ventana)

Report on noise certification level estimates of the final Ma 1.6 business jet studied in T5.2 delivered to WP6.

Key: CAEP 12 input (se abrirá en una nueva ventana)

Final agreed report of first project progress and plan of SENECA available to be presented to CAEP 12

Preliminary Exploitation & Dissemination Plan (EDP) (se abrirá en una nueva ventana)

Preliminary Exploitation Dissemination Plan EDP

Preliminary noise certification levels of Ma 1.6 business jet aircraft (se abrirá en una nueva ventana)

Report on noise certification level estimates for the preliminary status of the platform studied in T5.2 delivered to WP2, WP3 and WP6.

Preliminary CAEP 12 input (se abrirá en una nueva ventana)

Draft Report of first project results and presentation available for review with the project consortium and the advisory board

Final noise certification levels for Ma 1.4 business jet (se abrirá en una nueva ventana)

Report on noise certification level estimates of the final Ma 1.4 business jet studied in T5.1 delivered to WP6.

Overview of the certification projections for the HISAC project (se abrirá en una nueva ventana)

In Task 42 Overview of the certification projections for the HISAC project

Preliminary certification levels of Ma 1.4 business jet (se abrirá en una nueva ventana)

Report on noise certification level estimates for the preliminary status of the platform studied in T5.1 delivered to WP2, WP3 and WP6.

Assessment of previous studies of the impacts of supersonic aircraft (se abrirá en una nueva ventana)

In Task 45 Assessment of previous studies of the impacts of supersonic aircraft

Refined sensitivity study on climate impact of supersonic aviation (se abrirá en una nueva ventana)

In Task 4.5: Refined sensitivity study on climate impact of supersonic aviation

0D Contrails formation simulation with ice crystals for one configuration (se abrirá en una nueva ventana)

In Task 4.4: 0D Contrails formation simulation with ice crystals for one configuration

Publicaciones

Dual-Stream Jet Noise Test with Internal Mixer Design Variations for LTO Noise of Supersonic Aircraft

Autores: Remco Habing, Mark-Jan van der Meulen, Maxime Huet, Robert Jaron, Francesco Petrosino, Mattia Barbarino & Oleksandr Zaporozhets
Publicado en: ICAS 2024, 2024
Editor: ICAS 2024

Conceptual Design of a Next Generation Supersonic Airliner for Low Noise and Emissions (se abrirá en una nueva ventana)

Autores: Cristina Villena Munoz and Giordana Bonavolontà and Craig Lawson and Atif Riaz
Publicado en: AIAA SCITECH 2023 Forum, 2022
Editor: AIAA SCITECH 2023 Forum
DOI: 10.2514/6.2023-0215.c1

Aeroakustischer Vergleich eines Ein- und eines MehrstufigenFan-Konzepts für zivile überschallfähige Triebwerke (se abrirá en una nueva ventana)

Autores: M. Gräbert, R. Jaron, M. Plohr
Publicado en: DLRK, 2023
Editor: DLRK
DOI: 10.25967/610277

Local air quality assessment scenarios for new supersonic aircraft evaluation

Autores: K. Synylo, A.Krupko, O. Zaporozhets
Publicado en: Seminarium V New Trends in the Construction, Research and Operation of Flying Object, 2023
Editor: NAU

Design of The Seneca Mach 1.8 Supersonic Airliner with Multi-Fidelity Aerodynamic Analysis for Noise-Optimised Take-Off Trajectories

Autores: C. Villena Muñoz, C. Lawson, A. Riaz, A. Sharma
Publicado en: ICAS 2024, 2024
Editor: ICAS 2024

Jet Noise Prediction Benchmark for Landing and Takeoff Noise of Supersonic Aircraft (se abrirá en una nueva ventana)

Autores: Robert Jaron, Matti Gräbert,Remco Habing, Mark-Jan van der Meulen, Maxime Huet, Ingrid LeGriffon, Francesco Petrosino, Mattia Barbarino, Katharina Lefarth,Oleksandr Zaporozhets
Publicado en: InterNoise, 2022
Editor: InterNoise
DOI: 10.3397/in_2023_1064

Concorde noise model benchmarking for supersonic aircraft

Autores: K.Kazhan, V.Makarenko, V.Tokarev, O.Zaporozhets
Publicado en: Seminarium V New Trends in the Construction, Research and Operation of Flying Object, 2023
Editor: NAU

Reference aircraft noise model for the new supersonic airplane design with corrected noise propagation and engine installation effect contributions

Autores: Oleksandr Zaporozhets, Vitalii Makarenko, Vadim Tokarev, Kateryna Kazhan
Publicado en: ACASD, 2025
Editor: ACASD

Single- and Two-Stage Fan Designs for a Supersonic Airliner with Focus on Certification Noise Reduction (se abrirá en una nueva ventana)

Autores: Matti Graebert, Robert Jaron, Cristina Villena Munoz, Martin Plohr and Antoine Moreau
Publicado en: AIAA SciTech 2025, 2025
Editor: AIAA
DOI: 10.2514/6.2025-2680

Local Air Quality Studies for Supersonic Aircraft (se abrirá en una nueva ventana)

Autores: Kateryna Synylo, Andrii Krupko, Oleksandr Zanorozhets
Publicado en: 2024 New Trends in Aviation Development (NTAD), 2025, Página(s) 176-180
Editor: IEEE
DOI: 10.1109/ntad63796.2024.10850156

Numerical evaluation of jet noise with flight effect for supersonic civil aircraft using ZDES

Autores: Maxime Huet, Olivier Atinault, Fabien Gand, Hugo Demontis
Publicado en: AIAA Aviation Forum 2025, 2025
Editor: AIAA Aviation Forum 2025

Engine installation effect contribution in noise performances of the new supersonic airplane (se abrirá en una nueva ventana)

Autores: Oleksandr Zaporozhets, Vitalii Makarenko, Vadim Tokarev, Kateryna Kazhan
Publicado en: 2024 New Trends in Aviation Development (NTAD), 2025, Página(s) 230-235
Editor: IEEE
DOI: 10.1109/ntad63796.2024.10850272

Pollution Assessment at Airport Operational Scenario

Autores: K. Synylo, O. Zaporozhets, A. Krupko, K. Kazhan, V. Makarenko, V. Tokarev and S. Karpenko
Publicado en: International Symposium on Electric Aviation and Autonomous Systems, 2023, ISBN 978-83-63539-94-8
Editor: ISEAS

The Future of Cicil Supersonic Transport in Europe: The SENECA and MORE&LESS Projects

Autores: Robert Jaron, Nicole Viola
Publicado en: ICAS 2024, 2024
Editor: ICAS 2024

Intermodel comparison of the atmospheric composition changes due to emissions from a future supersonic aircraft fleet (se abrirá en una nueva ventana)

Autores: Jurriaan A. van 't Hoff, Didier Hauglustaine, Johannes Pletzer, Agnieszka Skowron, Volker Grewe, Sigrun Matthes, Maximilian M. Meuser, Robin N. Thor, Irene C. Dedoussi
Publicado en: 2024
Editor: Egusphere
DOI: 10.5194/egusphere-2024-2866

Desarrollo de un Modelo de Predicción de Emisiones para Turbinas de Gas de Aviación Basado en Redes de Reactores (se abrirá en una nueva ventana)

Autores: José María García Oliver, Jaime Gimeno García, Borja Martínez Corzo, Javier Navarro Laboulais, Pénélope Leyland
Publicado en: XV Congreso Iberoamericano de Ingeniería Mecánica, 2022
Editor: XV Congreso Iberoamericano de Ingeniería Mecánica
DOI: 10.5944/bicim2022.141

Promising Technologies to Reduce Aviation Noise at Airports

Autores: O. Zaporozhets, K. Kazhan, V. Makarenko, V. Tokarev, A. Chyla, M. Bukala
Publicado en: 9th European Congress on Computational Methods in Applied Sciences and Engineering, 2024
Editor: ECCOMAS

Conceptual Design of Supersonic Aircraft to Investigate Environmental Impact (se abrirá en una nueva ventana)

Autores: Cristina Villena Munoz, Craig Lawson, Atif Riaz, Robert Jaron
Publicado en: AIAA SCITECH 2024 Forum, 2024
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2024-2115

Use of semi-empirical models to predict jet noise radiated byunsuppressed and suppressed nozzles

Autores: Anthony Lafitte, Maxime Huet
Publicado en: InterNoise 2024, 2024
Editor: InterNoise 2024

Promising Technologies to Reduce Global and Local Aviation Emissions

Autores: K. Synylo, O. Zaporozhets , A. Krupko, S. Karpenko
Publicado en: ECCOMAS Congress 2024, 2024
Editor: ECCOMAS

SENECA project: Climate effects assessment of supersonic aviation

Autores: Etienne Terrenoire, Sigrun Matthes, Robin Thor, David Lee, Ruben Rodriguez de Leon, Ling Lim, Bethan Owen, Agnieska Skrowron, Pénélope Leyland, David Marsh and Kateryna Synylo
Publicado en: ECCOMAS 2022, 2022
Editor: ECCOMAS 2022

Preliminary design of next generation Mach 1.6 supersonic business jets to investigate landing & take-off (LTO) noise and emissions – SENECA

Autores: C. Mourouzidis, D. Del Gatto, S. Adamidis, C. Villena Munoz, C. Lawson, B. Martinez Corzo, P. Leyland, D. Marsh, L. Lim, B. Owen, E. Terrenoire, O. Atinault, I. LeGriffon, M. Huet, M. Schaefer, M. Plohr, S. Bake, P. Madden
Publicado en: 12th EASN International Conference, 2022
Editor: 12th EASN International Conference

Thermodynamic Design and Emissions Model of a Mach 1.8 Supersonic Airliner Engine

Autores: Martin Plohr, Sebastian Zenkner, Sebastian Bake, Dirk Zeitz
Publicado en: ICAS 2024, 2024
Editor: ICAS 2024

Landing and Takeoff Noise Prediction of Conceptual Supersonic Aircraft

Autores: M. Graebert, R. Jaron, M. Plohr, S. Zenkner, C. Richter, C. Stöhr, C. Villena Muñoz, M.-J. van der Meulen, R. Habing, M. Huet, F. Petrosino, M. Barbarino, F. Fischer & O. Zaporozhets
Publicado en: ICAS 2024, 2024
Editor: ICAS 2024

Near-filed mesh adaptation for contrail modeling of a supersonic aircraft

Autores: Mathieu Muller, Etienne Terrenoire
Publicado en: AERO 2023, 3AF, 2022
Editor: AERO 2023, 3AF

Comparison of analytical Semi-empirical model for Jet-noise Prediction

Autores: Francesco Petrosino, Mattia Barbarino
Publicado en: ICAS 2022, Edición ICAS2022_0885, 2022
Editor: ICAS

Novel Aircraft Emission and Fuel Burn Assessment Scenarios at Aircraft, Airport and Fleet Levels

Autores: K. Synylo, O. Zaporozhets, A. Krupko, K. Kazhan, V. Makarenko, V. Tokarev and S. Karpenko
Publicado en: International Symposium on Electric Aviation and Autonomous Systems, 2023, ISBN 978-83-63539-94-8
Editor: ISEAS

SENECA’s aircraft emissions evaluation and theirs environmental considerations

Autores: E. Terrenoire, M. Muller, E. Ramirez Correra, P. Leyland, K. Synylo, A. Krupko, O. Zaporozhets, D. Lee, B.Owen, L. Lim, A. Skowron, R. Rodriguez De Leon, D. Marsh, S. Matthes, P. Madden,S. Bake, C. Mourouzidis
Publicado en: ICAS 2024, 2024
Editor: ICAS 2024

Review: The Effects of Supersonic Aviation on Ozone and Climate (se abrirá en una nueva ventana)

Autores: Matthes, Sigrun; De Leon, Ruben; Lee, David,; De Leon, Ruben Rodriguez; Lim, Ling; Owen, Bethan; Skowron, Agnieszka; Thor, Robin; Terrenoire, Etienne
Publicado en: Aerospace, Edición 9, 2022, Página(s) 41, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/aerospace9010041

Review of Sonic Boom Prediction and Reduction Methods for Next Generation of Supersonic Aircraft (se abrirá en una nueva ventana)

Autores: Giordana Bonavolontà; Craig Lawson; Atif Riaz
Publicado en: Aerospace, Edición 4, 2023, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/aerospace10110917

Survey of Semi-Empirical Jet Noise Models for Preliminary Aircraft Engine Design (se abrirá en una nueva ventana)

Autores: Francesco Petrosino; Mattia Barbarino
Publicado en: Aerospace, 2023, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/aerospace10070625

Preliminary design of next generation Mach 1.6 supersonic business jets to investigate landing & take-off (LTO) noise and emissions – SENECA. (se abrirá en una nueva ventana)

Autores: Mourouzidis, C.; Del Gatto, D.; Adamidis, S.; Villena Munoz, C.; Lawson, C.; Martinez Corzo, B.; Leyland, P.; Marsh, D.; Lim, L.; Owen, B.; Terrenoire, E.; Atinault, O.; LeGriffon, I.; Huet, M.; Schaefer, M.; Plohr, M.; Bake, S.; Madden, P.
Publicado en: Journal of Physics: Conference Series, 2023, ISSN 1742-6596
Editor: IOPscience
DOI: 10.1088/1742-6596/2526/1/012011

Sensitivities of climate impact of supersonic aviation

Autores: Robin Thor, Agnieszka Skowron, Sigrun Matthes, Ruben Rodriguez De Leon
Publicado en: TAC5 conference, 2022
Editor: TAC5

The Effects of Supersonic Aviation on Ozone and Climate

Autores: Sigrun Matthes, David S. Lee, Ruben Rodriguez De Leon, Ling Lim, Bethan Owen, Agnieszka Skowron, Robin N. Thor, Etienne Terrenoire
Publicado en: TAC5 conference, 2022
Editor: TAC5

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