Shape Adaptive Blades for Rotorcraft Efficiency

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

D2.26 Wind tunnel test report

Wind tunnel test report

D3.18 Final Project Reporting (Minutes of meeting, Activity report, Management report)

Final Project Reporting (Minutes of meeting, Activity report, Management report)

D2.6 Model validation and final report on inertial twist

Model validation and final report on inertial twist

D3.12 Phase 2 Reporting (Minutes of checkpoint meeting, Activity report)

Phase 2 Reporting (Minutes of checkpoint meeting, Activity report)

D1.13 Updated morphing concept CFD polars delivered to T1.2

Updated morphing concept CFD polars delivered to T1.2

D1.4 S4 CA results on morphing performance

S4 CA results on morphing performance

D2.30 Final report on quasi-static passive energy balancing

Final report on quasi-static passive energy balancing

D1.14 Report on aeroacoustic performance of morphing concepts

Report on aeroacoustic performance of morphing concepts

D3.13 Critical Design Review (CDR)

Critical Design Review (CDR)

D2.25 Wind tunnel test proof load requirements

Wind tunnel test proof load requirements

D3.1 Partner List and copies of EC contract and Consortium Agreement.

Partner List and copies of EC contract and Consortium Agreement.

D3.15 Test Readiness Review (TRR)

Test Readiness Review (TRR)

D2.33 Helicopter preliminary design tool (initiator) report

Helicopter preliminary design tool (initiator) report

D2.31 Resonant actuation final report

Resonant actuation final report

D1.3 Decide common format for exchange of surrogate models

Decide common format for exchange of surrogate models

D1.5 Initial morphing concept design targets

Initial morphing concept design targets

D3.10 Report on dissemination and exploitation strategy

Report on dissemination and exploitation strategy

D1.1 Selection of baseline rotor

Selection of baseline rotor

D1.12 Initial morphing concept CFD polars delivered to T1.2

Initial morphing concept CFD polars delivered to T1.2

D2.34 Report on system level benefits of multi-functional morphing blades

Report on system level benefits of multi-functional morphing blades

D2.18 Model validation and final report on active tendons

Model validation and final report on active tendons

D3.11 Preliminary exploitation report

Preliminary exploitation report

D2.9 Model validation and final report on FishBAC

Model validation and final report on FishBAC

D3.17 Final report on Dissemination and Exploitation

Final report on Dissemination and Exploitation

D2.29 Interim report on negative stiffness design and optimisation

Interim report on negative stiffness design and optimisation

D3.2 Minutes of the Kick-Off meeting

Minutes of the Kick-Off meeting

D2.15 Model validation and final report on variable chord

Model validation and final report on variable chord

D1.9 Report of final high-fidelity CFD/CSD simulation results

Report of final high-fidelity CFD/CSD simulation results

D2.12 Model validation and final report on TRIC concept

Model validation and final report on TRIC concept

D2.28 Whirl tower test report

Whirl tower test report

D3.16 Phase 3 Reporting (Minutes of checkpoint meeting, Activity report)

Phase 3 Reporting (Minutes of checkpoint meeting, Activity report)

D1.2 Report on analytical adaptive rotor studies

Report on analytical adaptive rotor studies

D1.7 Refined blade design and morphing mechanism design targets

Refined blade design and morphing mechanism design targets

D3.8 Phase 1 Reporting (Minutes of checkpoint meeting, Activity report)

Phase 1 Reporting (Minutes of checkpoint meeting, Activity report)

D1.15 Optimized morphed rotor blade shapes for low noise

Optimized morphed rotor blade shapes for low noise

D2.32 Technology Compliance Matrix for morphing concepts

Technology Compliance Matrix for morphing concepts

D3.9 Preliminary Design Review (PDR)

Preliminary Design Review (PDR)

D2.3 Model validation and final report on SMA active twist

Model validation and final report on SMA active twist

D2.27 Whirl tower test proof load requirements

Whirl tower test proof load requirements

D2.22 TRIC wind tunnel and whirl tower test articles

TRIC wind tunnel and whirl tower test articles

D2.21 FishBAC wind tunnel and whirl tower test articles

FishBAC wind tunnel and whirl tower test articles

D2.20 Inertially driven twist whirl tower test article

Inertially driven twist whirl tower test article

D2.23 Variable chord wind tunnel and whirl tower test articles

Variable chord wind tunnel and whirl tower test articles

D2.19 SMA twist wind tunnel and whirl tower demonstrators

SMA twist wind tunnel and whirl tower demonstrators

D2.24 Active tendon whirl tower test article

Active tendon whirl tower test article

D1.11 Surrogate model of emissions versus rotor power required

Surrogate model of emissions versus rotor power required

D2.4 Initial surrogate model of inertial twist and report

Initial surrogate model of inertial twist and report

D2.17 Refined active tendon surrogate model

Refined active tendon surrogate model

D2.14 Refined surrogate model of variable chord extension

Refined surrogate model of variable chord extension

D2.2 Refined surrogate model of SMA active twist and report

Refined surrogate model of SMA active twist and report

D2.13 Initial surrogate model of variable chord extension

Initial surrogate model of variable chord extension

D2.5 Refined surrogate model of inertial twist and report

Refined surrogate model of inertial twist and report

D2.10 Initial surrogate model of TRIC concept

Initial surrogate model of TRIC concept

D2.11 Refined surrogate model of TRIC concept

Refined surrogate model of TRIC concept

D2.1 Initial surrogate model of SMA active twist and report

Initial surrogate model of SMA active twist and report

D1.10 Rotorcraft emissions model

Rotorcraft emissions model

D2.16 Initial active tendon surrogate model

Initial active tendon surrogate model

D1.8 Computed highly-resolved flow fields for T1.5

Computed highly-resolved flow fields for T1.5

D2.8 Refined surrogate model of FishBAC

Refined surrogate model of FishBAC

D2.7 Initial surrogate model of FishBAC

Initial surrogate model of FishBAC

D1.6 CFD/CSD coupled analysis running

CFD/CSD coupled analysis running

D3.5 Intra consortium website set up for SABRE

Intra consortium website set up for SABRE

D3.14 Special Session at AIAA Scitec Conference

Workshop on morphing rotorcraft at DLR Braunschweig - This deliverable has changed to Special Session at AIAA SciTech Conference in M32 - delivered the same intended outcomes as the session at Braunschweig cancelled due to COVID-19 pandemic

D3.3 SABRE Project Handbook

SABRE Project Handbook

D3.4 SABRE Project Overview Presentation

SABRE Project Overview Presentation

D3.19 Final project booklet of results

Final project booklet of results

D3.7 Project leaflet to identified stakeholders

Project leaflet to identified stakeholders

D3.6 Public website, LinkedIn profile, and ResearchGate profile set up

Public website, LinkedIn profile, and ResearchGate profile set up

Pubblicazioni

Linearly variable chord-extension morphing for helicopter rotor blades

Autori: Rohin K. Majeti, Berend G. van der Wall, Christoph G. Balzarek
Pubblicato in: CEAS Aeronautical Journal, Numero 15 Oct 2020, 2020, Pagina/e 00477-4, ISSN 1869-5582
Editore: Springer Science + Business Media
DOI: 10.1007/s13272-020-00477-4

Passive energy balancing design for a linear actuated morphing wingtip structure

Autori: Jiaying Zhang, Chen Wang, Alexander D. Shaw, Mohammadreza Amoozgar, Michael I. Friswell
Pubblicato in: Aerospace Science and Technology, Numero 107, 2020, Pagina/e 106279, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2020.106279

Aeroelastic model and analysis of an active camber morphing wing

Autori: Jiaying Zhang, Alexander D. Shaw, Chen Wang, Huaiyuan Gu, Mohammadreza Amoozgar, Michael I. Friswell, Benjamin K.S. Woods
Pubblicato in: Aerospace Science and Technology, Numero 111, 2021, Pagina/e 106534, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2021.106534

Structural Modeling of Compliance-Based Camber Morphing Structures Under Transverse Shear Loading

Autori: Andres E. Rivero, Paul M. Weaver, Jonathan E. Cooper, Benjamin K. S. Woods
Pubblicato in: AIAA Journal, Numero 58/11, 2020, Pagina/e 4941-4951, ISSN 0001-1452
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.J058842

Linearly variable chord-extension morphing for helicopter rotor blades

Autori: Rohin K. Majeti, Berend G. van der Wall, Christoph G. Balzarek
Pubblicato in: CEAS Aeronautical Journal, Numero 12/1, 2021, Pagina/e 55-67, ISSN 1869-5582
Editore: Springer Science + Business Media
DOI: 10.1007/s13272-020-00477-4

The effect of curved tips on the dynamics of composite rotor blades

Autori: M.R. Amoozgar, A.D. Shaw, M.I. Friswell
Pubblicato in: Aerospace Science and Technology, Numero 106, 2020, Pagina/e 106197, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2020.106197

Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps

Autori: Andres E. Rivero, Stephane Fournier, Marinos Manolesos, Jonathan E. Cooper, Benjamin K. S. Woods
Pubblicato in: AIAA Journal, Numero Monthly, 2021, Pagina/e 1-14, ISSN 0001-1452
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.j059606

Bidirectional torsional negative stiffness mechanism for energy balancing systems

Autori: Jiaying Zhang, Alexander D. Shaw, Mohammadreza Amoozgar, Michael I. Friswell, Benjamin K.S. Woods
Pubblicato in: Mechanism and Machine Theory, Numero 131, 2019, Pagina/e 261-277, ISSN 0094-114X
Editore: Pergamon Press Ltd.
DOI: 10.1016/j.mechmachtheory.2018.10.003

The effect of a movable mass on the aeroelastic stability of composite hingeless rotor blades in hover

Autori: M.R. Amoozgar, A.D. Shaw, J. Zhang, M.I. Friswell
Pubblicato in: Journal of Fluids and Structures, Numero 87, 2019, Pagina/e 124-136, ISSN 0889-9746
Editore: Academic Press
DOI: 10.1016/j.jfluidstructs.2019.03.017

Lag-twist coupling sensitivity and design for a composite blade cross-section with D-spar

Autori: M.R. Amoozgar, A.D. Shaw, J. Zhang, C. Wang, M.I. Friswell
Pubblicato in: Aerospace Science and Technology, Numero 91, 2019, Pagina/e 539-547, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2019.05.053

Bidirectional Spiral Pulley Negative Stiffness Mechanism for Passive Energy Balancing

Autori: Jiaying Zhang, Alexander D. Shaw, Mohammadreza Amoozgar, Michael I. Friswell, Benjamin K. S. Woods
Pubblicato in: Journal of Mechanisms and Robotics, Numero 11/5, 2019, ISSN 1942-4302
Editore: American Society of Mechanical Engineers
DOI: 10.1115/1.4043818

Composite Blade Twist Modification by Using a Moving Mass and Stiffness Tailoring

Autori: M. R. Amoozgar, A. D. Shaw, J. Zhang, M. I. Friswell
Pubblicato in: AIAA Journal, Numero 57/10, 2019, Pagina/e 4218-4225, ISSN 0001-1452
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.j057591

Free vibration analysis of a rotating pre-twisted beam subjected to tendon-induced axial loading

Autori: V. Ondra, B. Titurus
Pubblicato in: Journal of Sound and Vibration, Numero 461, 2019, Pagina/e 114912, ISSN 0022-460X
Editore: Academic Press
DOI: 10.1016/j.jsv.2019.114912

Theoretical and experimental free vibration analysis of a beam-tendon system with an eccentrically placed tendon

Autori: V. Ondra, B. Titurus
Pubblicato in: Thin-Walled Structures, Numero 144, 2019, Pagina/e 106347, ISSN 0263-8231
Editore: Elsevier BV
DOI: 10.1016/j.tws.2019.106347

Theoretical and experimental modal analysis of a beam-tendon system

Autori: V. Ondra, B. Titurus
Pubblicato in: Mechanical Systems and Signal Processing, Numero 132, 2019, Pagina/e 55-71, ISSN 0888-3270
Editore: Academic Press
DOI: 10.1016/j.ymssp.2019.06.016

Twist morphing of a composite rotor blade using a novel metamaterial

Autori: Huaiyuan Gu, Alexander D. Shaw, Mohammadreza Amoozgar, Jiaying Zhang, Chen Wang, Michael I. Friswell
Pubblicato in: Composite Structures, Numero 254, 2020, Pagina/e 112855, ISSN 0263-8223
Editore: Elsevier BV
DOI: 10.1016/j.compstruct.2020.112855

Modal analysis of a rotating pre-twisted beam axially loaded by an internally guided tendon

Autori: Jun Wu, Branislav Titurus
Pubblicato in: Journal of Sound and Vibration, Numero January 2021, 2021, Pagina/e 115980, ISSN 0022-460X
Editore: Academic Press
DOI: 10.1016/j.jsv.2021.115980

Effect of active camber morphing on rotor performance and control loads

Autori: Dominik Komp, Sumeet Kumar, Manfred Hajek, Jürgen Rauleder
Pubblicato in: Aerospace Science and Technology, Numero 108, 2021, Pagina/e 106311, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2020.106311

A shape memory alloy torsion actuator for static blade twist

Autori: Salvatore Ameduri, Antonio Concilio
Pubblicato in: Journal of Intelligent Material Systems and Structures, Numero 30/17, 2019, Pagina/e 2605-2626, ISSN 1045-389X
Editore: SAGE Publications
DOI: 10.1177/1045389x19873396

Free vibration and stability analysis of a cantilever beam axially loaded by an intermittently attached tendon

Autori: V. Ondra, B. Titurus
Pubblicato in: Mechanical Systems and Signal Processing, Numero 158, 2021, Pagina/e 107739, ISSN 0888-3270
Editore: Academic Press
DOI: 10.1016/j.ymssp.2021.107739

Active and Passive Camber Morphing for Helicopter Rotors towards PerformanceImprovements in Hover and Vertical Flight

Autori: Kushagra Vidyarthi, Yasir Zahoor, Roeland De Breuker, Marilena Pavel, Mark Voskuijl
Pubblicato in: Proceedings of VFS International 76th Annual Forum, Numero 6-8 October 2020, 2020
Editore: Vertical Flight Society

Manufacturing and characterisation of a composite FishBAC morphing wind tunnel model

Autori: Andres E Rivero, Stephane Fournier, Paul Weaver, Jonathan Cooper, Benjamin King Sutton Woods
Pubblicato in: ICAST 2018: 29th International Conference on Adaptive Structures, Numero Annual, 2018, Pagina/e 1-14
Editore: International Conference on Adaptive Structures and Technologies

Effect of Active Camber on Rotor Noise, Power and Hub Vibration

Autori: Sumeet Kumar, Dominik Komp, Manfred Hajek, Juergen Rauleder
Pubblicato in: AIAA Scitech 2021 Forum, Numero January 2021, 2021, ISBN 978-1-62410-609-5
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-1927

Rotor Performance Enhancements with Spanwise Varying Active Camber Morphing

Autori: Dominik Komp, Manfred Hajek, Juergen Rauleder
Pubblicato in: AIAA Scitech 2021 Forum, Numero January 2021, 2021, ISBN 978-1-62410-609-5
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-0200

Development of a conceptual demonstrator of a SMA-based Rotorcraft blade twist system

Autori: Antonio Concilio; Salvatore Ameduri; Bernardino Galasso; Antonio Gianvito
Pubblicato in: isbn: 9781510625853, Numero 1, 2019
Editore: SPIE Digital Library
DOI: 10.1117/12.2511963

Shape memory alloys compact actuators for aerodynamic surfaces twisting

Autori: Salvatore Ameduri; Bernardino Galasso; Monica Ciminello; Antonio Concilio
Pubblicato in: AIAA Scitech 2020 Forum, Numero 3, 2020
Editore: AIAA
DOI: 10.2514/6.2020-1299

Spiral Pulley Negative Stiffness Mechanism for Morphing Aircraft Actuation

Autori: Jiaying Zhang, Alexander D. Shaw, Amoozgar Mohammadreza, Michael I. Friswell, Benjamin K. S. Woods
Pubblicato in: Volume 5B: 42nd Mechanisms and Robotics Conference, Numero 26-29 August 2018, 2018, Pagina/e V05BT07A003, ISBN 978-0-7918-5181-4
Editore: ASME
DOI: 10.1115/DETC2018-85640

Cross-sectional design of a composite rotor blade for twist morphing

Autori: MR Amoozgar, AD Shaw, J Zhang & MI Friswell
Pubblicato in: 6th Aircraft Structural Design Conference, Numero 9-11 October 2018, 2018
Editore: Royal Aeronautical Society

Torsional Negative Stiffness Mechanism for Bidirectional Morphing Aircraft Actuation

Autori: J Zhang, AD Shaw, MR Amoozgar, MI Friswell & BKS Woods
Pubblicato in: 6th Aircraft Structural Design Conference, Numero 9-11 October 2018, 2018
Editore: Royal Aeronautical Society

Twist morphing of a hingeless rotor blade using a moving mass

Autori: MR Amoozgar, AD Shaw, J Zhang & MI Friswell
Pubblicato in: 44th European Rotorcraft Forum, Numero 18-21 September 2018, 2018
Editore: European Rotorcraft Forum

Static aeroelastic response of a rotor blade under internal axial loading

Autori: R. Dibble, BKS Woods, B. Titurus
Pubblicato in: 43rd European Rotorcraft Forum, Numero 12-14 September 2017, 2017
Editore: European Rotorcraft Forum

Towards an application of an active tendon in rotorcraft: A numerical and experimental study of coupled bending-torsion vibration of a beam-tendon system

Autori: V. Ondra, R. Dibble, B. Titurus
Pubblicato in: 28th International Conference on Noise and Vibration engineering (ISMA2018), Numero 17 September 2018, 2018, ISBN 9789-073802995
Editore: ISMA

Hoplite - a conceptual design environment for helicopters incorporating morphing rotor technology

Autori: K. Vidyarthi, M. Beuker, F. Yin, M. Voskuijl, M. Pavel
Pubblicato in: 44th European Rotorcraft Forum, Numero 18-21 September 2018, 2018
Editore: European Rotorcraft Forum

Mission-based optimal morphing parameters for Rotors with combined chord and twist morphing

Autori: R. K. Majeti, S. Benz
Pubblicato in: 8th Asian/Australian Rotorcraft Forum, Numero 30 Oct - 02 Nov 2019, 2019
Editore: ARF

An advanced surrogate model for predicting the Impact of SMA twist system on the helicopter performance.

Autori: S. Ameduri, A. Concilio, R K Majeti
Pubblicato in: ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Numero 9-11 September 2019, 2019
Editore: American Society of Mechanical Engineers

Optimization of a Rotor with Morphing Blades using Particle Swarm Algorithm

Autori: S. Benz, R. K. Majeti
Pubblicato in: Deutscher Luft und Raumfahrtkongress 2019, Numero 30 September - 2 October, 2019
Editore: DGLR

Linearly Variable Chord-Extension Morphing for Helicopter Rotor Blades. I

Autori: Majeti, Rohin Kumar und van der Wall, Berend G. und Balzarek, Christoph
Pubblicato in: Vertical Flight Society 75th Annual Forum, Numero 13.-16. May 2019, 2019
Editore: VFS

Chord Morphing for Helicopter Rotor Blades

Autori: Johannes Riemenschneider, Christoph Balzarek, Berend G. van der Wall, Rohin Kumar Majeti
Pubblicato in: ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Numero 9-11 September 2019, 2019, ISBN 978-0-7918-5913-1
Editore: American Society of Mechanical Engineers
DOI: 10.1115/smasis2019-5625

Wind Tunnel Comparison of Flapped and FishBAC Camber Variation for Lift Control

Autori: Andres E. Rivero, Stephane Fournier, Marinos Manolesos, Jonathan E. Cooper, Benjamin Woods
Pubblicato in: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1300

Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures

Autori: Andres E. Rivero, Jonathan E. Cooper, Benjamin Woods
Pubblicato in: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1298

Surrogate Modelling of the Steady Aeroelastic Performance of the Fish Bone Active Camber Concept

Autori: Stephane Fournier, Benjamin K. Woods
Pubblicato in: AIAA Scitech 2019 Forum, Numero Yearly, 2019, Pagina/e 1-12, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1859

Structural Modelling of Compliance-Based Morphing Structures under Transverse Shear Loading

Autori: Andres E. Rivero, Paul Weaver, Benjamin K. Woods
Pubblicato in: AIAA Scitech 2019 Forum, Numero Yearly, 2019, Pagina/e 1-17, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-0229

Tailored Nonlinear Negative Stiffness Mechanisms for Linear Motion

Autori: J Zhang, AD Shaw, C Wang, MR Amoozgar, MI Friswell
Pubblicato in: IX ECCOMAS Thematic Conference on Smart Structures and Materials, Numero 8-12 June 2019, 2019, Pagina/e 473-484, ISBN 978-84-949194-6-6
Editore: International Centre for Numerical Methods in Engineering (CIMNE), Barcelona, Spain

Integration of the Spiral Pulley Negative Stiffness Mechanism into the FishBAC Morphing Wing

Autori: C Wang, J Zhang, AD Shaw, MR Amoozgar, MI Friswell, BKS Woods
Pubblicato in: IX ECCOMAS Thematic Conference on Smart Structures and Materials, Numero 8-12 July 2019, 2019, Pagina/e 452-461, ISBN 978-84-949194-6-6
Editore: International Centre for Numerical Methods in Engineering (CIMNE), Barcelona, Spain

Performance Analysis of Inertial Twist Morphing Concept in Hovering Flight

Autori: MR Amoozgar, AD Shaw, J Zhang, C Wang, MI Friswell
Pubblicato in: 45th European Rotorcraft Forum 2019 (ERF), Numero 17-20 September 2019, 2019
Editore: Warsaw Univeristy of Technology

Passive Energy Balancing for Morphing Rotorcraft Actuation: Integration and optimisation

Autori: Chen Wang, Jiaying Zhang, Mohammadreza Amoozgar, Alex Shaw, Michael Ian Friswell, Benjamin Woods
Pubblicato in: AIAA Scitech 2020 Forum, Numero 6-10 January 2020, 2020, Pagina/e Paper AIAA 2020-1303, ISBN 978-1-62410-595-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1303

Aerodynamic Performance of Morphing Blades and Rotor Systems

Autori: Rauleder, Jürgen; van der Wall, Berend G.; Woods, Benjamin K.S.; de Breuker, Roeland
Pubblicato in: AHS 74th Annual forum & Technology Display, Numero 14.-17. Mai 2018, 2018
Editore: American Helicotper Society International

Integrated Rotor Performance Improvement and Vibration Reduction Using Active Camber Morphing

Autori: Sumeet Kumar, Dominik Komp, Manfred Hajek, Jürgen Rauleder
Pubblicato in: ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Numero 9-11 September 2019, 2019, ISBN 978-0-7918-5913-1
Editore: American Society of Mechanical Engineers
DOI: 10.1115/smasis2019-5588

Numerical Investigation of the Effects of Dynamic Camber Variation on the Airfoil Characteristics of a Pitching Rotor Airfoil

Autori: Amine Abdelmoula, Stefan Platzer, Manfred Hajek, Juergen Rauleder
Pubblicato in: AIAA Scitech 2020 Forum, Numero 6-10 January 2020, 2020, ISBN 978-1-62410-595-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1302

Investigation of Active Rotor Design and Control for Performance Improvement

Autori: Komp D, Kumar S, Abdelmoula A, Hajek M, Rauleder J.
Pubblicato in: Vertical Flight Society 75th Annual Forum & Technology DisplayAt: Philadelphia, Pennsylvania, Numero May 2019, 2019
Editore: AHS International

Aerodynamic Performance of Morphed Camber Rotor Airfoils

Autori: Amine Abdelmoula, Juergen Rauleder
Pubblicato in: AIAA Scitech 2019 Forum, Numero 7-11 January 2019, 2019, ISBN 978-1-62410-578-4
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1101

Preliminary Design of a TE Morphing Surface for Rotorcraft

Autori: Yasir Zahoor, Roeland De Breuker, Mark Voskuijl
Pubblicato in: AIAA Scitech 2020 Forum, Numero January 2020, 2020, ISBN 978-1-62410-595-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1301

Effects of material and geometrical parameters on the design of a trailing edge camber morphing surface

Autori: Yasir Zahoor, Roeland De Breuker
Pubblicato in: Proceedings 2020 (Aerospace Europe Conference AEC2020, Numero 25-28 February 2020, 2020
Editore: 3AF

The Aerodynamics of Active Camber

Autori: Benjamin King Sutton Woods
Pubblicato in: 28th ICAST conference, Numero 9-13 October 2017, 2017
Editore: ICAST
DOI: 10.13140/rg.2.2.14104.70405

Aerodynamic Performance of Morphing Blades and Rotor Systems

Autori: Juergen Rauleder; Van Der Wall, B. G.; Abdelmoula, A.; Komp, D.; Kumar, S.; Ondra, V.; Titurus, B.; Woods, B. K. S.
Pubblicato in: Scopus - Elsevier, Numero 1, 2018
Editore: Elsevier

È in corso la ricerca di dati su OpenAIRE...

Risultati finali

Pubblicazioni

Condividi questa pagina Condividi questa pagina sui social network

Scarica Scarica il contenuto della pagina