Large Passenger Aircraft

STUDIES ON CELLULAR- BASED ADDITIVE MANUFACTURING PANELS AS ENABLERS OF SPECIFIC STIFFNESS REQUIREMENTS

Autori: Dr. Miguel Á. Castillo Acero; Dr. Federico Martín de la Escalera
Pubblicato in: 2017
Editore: EASN
DOI: 10.5281/zenodo.3907733

Desarrollos tecnológicos de Aernnova en Clean Sky 2, H2020

Autori: Miguel Angel Castillo
Pubblicato in: MATCOMP17 (Composite Materials 2017), 2017
Editore: MATCOMP
DOI: 10.5281/zenodo.3907668

Morphing Rudder

Autori: Castillo Acero, Miguel Á.; Cuerno, Cristina; Gómez-Tiermo, Miguel A.
Pubblicato in: 6th EASN conference, 2016
Editore: EASN
DOI: 10.5281/zenodo.3907458

Morphed vertical tailplane assessment for certification requirements

Autori: Castillo-Acero, Miguel Angel (Aernnova)
Pubblicato in: 5th CEAS Air & Space Conference, 2015
Editore: CEAS
DOI: 10.5281/zenodo.3905084

Assessment of T-tail flutter using an enhanced potential flow theory approach and linearized frequency domain CFD data

Autori: Schäfer, Dominik; Arnold, Jürgen
Pubblicato in: International Forum on Aeroelasticity and Structural Dynamics 2019, IFASD 2019, 2019
Editore: International Forum on Aeroelasticity and Structural Dynamics

Electrification Studies of Single Aisle Aircraft: A ‘Retrofit’ Investigation Including Parallel Hybrid Electric Propulsion

Autori: Wim Lammen, Jos Vankan
Pubblicato in: 2019
Editore: ISSA

CS2 Large Aircraft Disruptive Cockpit Demonstrator

Autori: FAGOT, Jean Jacques
Pubblicato in: CS2 General Conference 2019, 2019
Editore: CSJU
DOI: 10.5281/zenodo.6637620

Clean Sky contributions to aircraft life cycle reduction on emissions. Aernnova participation

Autori: Dr. Miguel Á. Castillo
Pubblicato in: Basque Ecodesign Meeting 2017, IHOBE, 2017
Editore: Ihobe
DOI: 10.5281/zenodo.3907833

Workload and Symbology workshop

Autori: Mark Nicols, Dave Moore, Mark Wilkins
Pubblicato in: 2018
Editore: BAES
DOI: 10.5281/zenodo.5560315

A 3D Continuum Damage Model for Tough Fibre Reinforced Polymer Composites Using Cuntze's Failure Mode Concept

Autori: Völkerink, Oliver; Petersen, Enno; Hühne, Christian
Pubblicato in: Numero 1, 2019
Editore: VI International Conference on Computational Modeling of Fracture and Failure of Materials and Structures

Aerodynamic Interaction Effects of Tip-Mounted Propellers Installed on the Horizontal Tailplane

Autori: Nando v. Arnhem, Tomas Sinnige, Tom C. Stokkermans, Georg Eitelberg, Leo L. Veldhuis
Pubblicato in: 2018 AIAA Aerospace Sciences Meeting, 2018, ISBN 978-1-62410-524-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-2052

A Real-life, French-accented Corpus of Air Traffic Control Communications

Autori: Estelle Delpech, Marion Laignelet, Christophe Pimm, Céline Raynal, Michal Trzos, Alexandre Arnold, Dominique Pronto
Pubblicato in: Language Resources and Evaluation Conference, 2018, ISBN 979-10-95546-00-9
Editore: ELRA

A Novel Human Machine Interface to Support Supervision and Guidance of Multiple Highly Automated Unmanned Aircraft

Autori: Max Friedrich, Joonas Lieb
Pubblicato in: 2019 IEEE/AIAA 38th Digital Avionics Systems Conference (DASC), 2019, Pagina/e 1-7, ISBN 978-1-7281-0649-6
Editore: IEEE
DOI: 10.1109/dasc43569.2019.9081645

Aerodynamic Investigation of an Over-the-Wing Propeller for Distributed Propulsion

Autori: Emanuel A. Marcus, Reynard de Vries, Akshay Raju Kulkarni, Leo L. Veldhuis
Pubblicato in: 2018 AIAA Aerospace Sciences Meeting, 2018, ISBN 978-1-62410-524-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-2053

A Preliminary Sizing Method for Hybrid-Electric Aircraft Including Aero-Propulsive Interaction Effects

Autori: Reynard de Vries, Malcom T. Brown, Roelof Vos
Pubblicato in: 2018 Aviation Technology, Integration, and Operations Conference, 2018, ISBN 978-1-62410-556-2
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-4228

"""Efficient simulation of the through-the-thickness damage composition in composite aircraft structures for use with integrated SHM systems"" (9th International Conference on Computational Methods; ICCM 2018)"

Autori: M. Garbade
Pubblicato in: 9th International Conference on Computational Methods; ICCM 2018, 2018
Editore: DLR

Conceptual Assessment of Hybrid Electric Aircraft with Distributed Propulsion and Boosted Turbofans

Autori: Maurice Hoogreef, Roelof Vos, Reynard de Vries, Leo L. Veldhuis
Pubblicato in: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1807

Preliminary Sizing of a Hybrid-Electric Passenger Aircraft Featuring Over-the-Wing Distributed-Propulsion

Autori: Reynard de Vries, Maurice Hoogreef, Roelof Vos
Pubblicato in: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1811

Aerodynamic Performance of an Aircraft Equipped with Horizontal Tail Mounted Propellers

Autori: Nando van Arnhem, Reynard de Vries, Roelof Vos, Leo L. Veldhuis
Pubblicato in: AIAA Aviation 2019 Forum, 2019, ISBN 978-1-62410-589-0
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3036

"""Manufacturing and reinforcement technologies for the next generation aircraft rear-end"" (Deutscher Luft- und Raumfahrt Kongress (DLRK))"

Autori: Yves Toso, Marc Garbade, Julian Adam, Andreas Kolbe, Thomas Haase
Pubblicato in: Deutscher Luft- und Raumfahrt Kongress (DLRK) 2019, 2019
Editore: Deutsche Gesellschaft für Luft- und Raumfahrt
DOI: 10.25967/490082

"""SELECTED CURRENT CHALLENGES IN THE DEVELOPMENT OF HYBRID LAMINAR FLOW CONTROL ON TRANSPORT AIRCRAFT"" (Deutscher Luft- und Raumfahrtkongress 2019)"

Autori: Ahmad Ali Pohya
Pubblicato in: Deutscher Luft- und Raumfahrt Kongress (DLRK) 2019, 2019
Editore: Deutsche Gesellschaft für Luft- und Raumfahrt (DGLR)
DOI: 10.25967/490089

An Impact Assessment of Degrading Elements on the Overall Benefit of Aircraft with Hybrid Laminar Flow Control

Autori: Ahmad A. Pohya, Kai Wicke
Pubblicato in: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1589

Design of a SW Framework for an Autopilot with Automated Test Capabilities on an Experimental Mid-Sized UAS

Autori: Ettore De Lellis, Federico Corraro, Gianluigi Di Capua, Luca Garbarino, Nicola Genito, Riccardo Rocchio
Pubblicato in: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-2381

Aerodynamic Interaction Between an Over-the-Wing Propeller and the Wing Boundary-Layer in Adverse Pressure Gradients

Autori: Reynard de Vries, Nando van Arnhem, Francesco Avallone, Daniele Ragni, Roelof Vos, Georg Eitelberg, Leo L. Veldhuis
Pubblicato in: AIAA Aviation 2019 Forum, 2019, ISBN 978-1-62410-589-0
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3035

Degree of similitude estimation for sub-scale flight testing

Autori: Akshay Raju Kulkarni, Gianfranco La Rocca, Leo L. Veldhuis
Pubblicato in: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1208

"""DLR Engagement in European Clean Sky-2 projects: a snapshot status"" (DLRK, German Aerospace Congress)"

Autori: U. Herrmann
Pubblicato in: German Aerospace Congress (DLRK), 2019
Editore: Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
DOI: 10.5281/zenodo.3897236

"""Numerical analysis and assessment of thermoplastically welded joints"" (International Conference on Lightweight Materials and Manufacture, LMM2019)"

Autori: Kreikemeier, J.; Abdulkadir, A.
Pubblicato in: International Conference on Lightweight Materials and Manufacture, LMM2019, 2019
Editore: tbd
DOI: 10.5281/zenodo.3898176

Real-Time Impact Identification by Using Acceleration Measurements—Application to a Large Aircraft Composite Panel

Autori: DIMITRI GOUTAUDIER, DIDIER GENDRE
Pubblicato in: Structural Health Monitoring 2019, 2019, ISBN 978-1-60595-601-5
Editore: DEStech Publications, Inc.
DOI: 10.12783/shm2019/32109

"""An Automation Language for Increasing Repeatability in Scaled Flight Testing of New Aircraft Configurations"" (8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS))"

Autori: R. Rocchio, F. Corraro, G. Di Capua, L. Garbarino, N. Genito
Pubblicato in: 2019
Editore: EUCASS
DOI: 10.13009/eucass2019-302

Conceptual Design Studies of Short Range Aircraft Configurations with Hybrid Electric Propulsion

Autori: Michael Iwanizki, Max Arzberger, Martin Plohr, Daniel Silberhorn, Tobias Hecken
Pubblicato in: AIAA Aviation 2019 Forum, 2019, ISBN 978-1-62410-589-0
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3680

Efficient simulation of multiple impact on double-curved composite structures

Autori: Marc Garbade, Caroline Wolff
Pubblicato in: 20th International Conference on Composite Structures, 2017
Editore: Structural and Computational Mechanics
DOI: 10.15651/978-88-938-5041-4

Virtual testing for design and certification of (fusion) bonded longitudinal joints in a fibre composite fuselage: A proposal using FEM-based progressive damage analysis

Autori: Völkerink, Oliver; Hühne, Christian
Pubblicato in: Composites Part C: Open Access, Numero Volume 7, 2022, ISSN 2666-6820
Editore: Elsevier B.V.
DOI: 10.1016/j.jcomc.2022.100236

Improved Analytical Prediction of Boundary-Layer induced Rotor Noise using Circumferential Modes

Autori: Martin Staggat, Antoine Moreau, Sebastien Guerin
Pubblicato in: Noise Control Engineering Journal (NCEJ), 2019, ISSN 0736-2501
Editore: Institute of Noise Control Engineering

Wingtip-Mounted Propellers: Aerodynamic Analysis of Interaction Effects and Comparison with Conventional Layout

Autori: Tomas Sinnige, Nando van Arnhem, Tom C. A. Stokkermans, Georg Eitelberg, Leo L. M. Veldhuis
Pubblicato in: Journal of Aircraft, Numero 56/1, 2019, Pagina/e 295-312, ISSN 0021-8669
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.c034978

Fan design assessment for BLI propulsion systems

Autori: M. Mennicken; D. Schoenweitz; M. Schnoes; R. Schnell
Pubblicato in: CEAS Aeronautical Journal, Numero 13, 2020, ISSN 1869-5582
Editore: Springer Science + Business Media
DOI: 10.1007/s13272-021-00532-8

Highly orthotropic panels structural stability, Farrar and Blochwaves theory

Autori: Miguel Ángel Castillo Acero
Pubblicato in: International Journal of Structural Integrity, Numero Vol. 8 (Numero 5)., 2017, Pagina/e pp.585-602, ISSN 1757-9864
Editore: Emerald Group Publishing Ltd.
DOI: 10.5281/zenodo.3907562

Strength prediction of adhesively bonded single lap joints with the eXtended Finite Element Method

Autori: O. Völkerink, J. Kosmann, M. J. Schollerer, D. Holzhüter, C. Hühne
Pubblicato in: The Journal of Adhesion, Numero 95/5-7, 2019, Pagina/e 474-494, ISSN 0021-8464
Editore: Taylor & Francis
DOI: 10.1080/00218464.2018.1553120

Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft

Autori: Reynard de Vries, Malcom Brown, Roelof Vos
Pubblicato in: Journal of Aircraft, Numero 56/6, 2019, Pagina/e 2172-2188, ISSN 1533-3868
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.c035388

"""Research Suggests A320 Mission Difficult for Distributed Hybrid-Electric"" (Aviation Week)"

Autori: Graham Warwick
Pubblicato in: Aviation Week, 2019
Editore: tbd

"""HLFC HTP - Hybrid laminar flow control at the horizontal tail plane"" (DLR Innovation Report 2019 - Institute of Composite Structures and Adaptive Systems)"

Autori: Markus Kleineberg, Andreas Schröder, Thomas Haase
Pubblicato in: Innovation Report 2019: Institute of Composite Structures and Adaptive Systems (DLR), Numero Annual, 2019, Pagina/e 42-43
Editore: Deutsches Zentrum für Luft- und Raumfahrt e.V.

Network Re-analysis of Boeing 737 Accident at Kegworth Using Different Potential Crewing Configurations for a Single Pilot Commercial Aircraft

Autori: Don Harris
Pubblicato in: Engineering Psychology and Cognitive Ergonomics, Numero 10906, 2018, Pagina/e 572-582, ISBN 978-3-319-91121-2
Editore: Springer International Publishing
DOI: 10.1007/978-3-319-91122-9_46

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