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Shape Adaptive Blades for Rotorcraft Efficiency

CORDIS provides links to public deliverables and publications of HORIZON projects.

Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .

Deliverables

D2.26 Wind tunnel test report (opens in new window)

Wind tunnel test report

D3.18 Final Project Reporting (Minutes of meeting, Activity report, Management report) (opens in new window)

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

D2.6 Model validation and final report on inertial twist (opens in new window)

Model validation and final report on inertial twist

D3.12 Phase 2 Reporting (Minutes of checkpoint meeting, Activity report) (opens in new window)

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

D1.13 Updated morphing concept CFD polars delivered to T1.2 (opens in new window)

Updated morphing concept CFD polars delivered to T1.2

D1.4 S4 CA results on morphing performance (opens in new window)

S4 CA results on morphing performance

D2.30 Final report on quasi-static passive energy balancing (opens in new window)

Final report on quasi-static passive energy balancing

D1.14 Report on aeroacoustic performance of morphing concepts (opens in new window)

Report on aeroacoustic performance of morphing concepts

D3.13 Critical Design Review (CDR) (opens in new window)

Critical Design Review (CDR)

D2.25 Wind tunnel test proof load requirements (opens in new window)

Wind tunnel test proof load requirements

D3.1 Partner List and copies of EC contract and Consortium Agreement. (opens in new window)

Partner List and copies of EC contract and Consortium Agreement.

D3.15 Test Readiness Review (TRR) (opens in new window)

Test Readiness Review (TRR)

D2.33 Helicopter preliminary design tool (initiator) report (opens in new window)

Helicopter preliminary design tool (initiator) report

D2.31 Resonant actuation final report (opens in new window)

Resonant actuation final report

D1.3 Decide common format for exchange of surrogate models (opens in new window)

Decide common format for exchange of surrogate models

D1.5 Initial morphing concept design targets (opens in new window)

Initial morphing concept design targets

D3.10 Report on dissemination and exploitation strategy (opens in new window)

Report on dissemination and exploitation strategy

D1.1 Selection of baseline rotor (opens in new window)

Selection of baseline rotor

D1.12 Initial morphing concept CFD polars delivered to T1.2 (opens in new window)

Initial morphing concept CFD polars delivered to T1.2

D2.34 Report on system level benefits of multi-functional morphing blades (opens in new window)

Report on system level benefits of multi-functional morphing blades

D2.18 Model validation and final report on active tendons (opens in new window)

Model validation and final report on active tendons

D3.11 Preliminary exploitation report (opens in new window)

Preliminary exploitation report

D2.9 Model validation and final report on FishBAC (opens in new window)

Model validation and final report on FishBAC

D3.17 Final report on Dissemination and Exploitation (opens in new window)

Final report on Dissemination and Exploitation

D2.29 Interim report on negative stiffness design and optimisation (opens in new window)

Interim report on negative stiffness design and optimisation

D3.2 Minutes of the Kick-Off meeting (opens in new window)

Minutes of the Kick-Off meeting

D2.15 Model validation and final report on variable chord (opens in new window)

Model validation and final report on variable chord

D1.9 Report of final high-fidelity CFD/CSD simulation results (opens in new window)

Report of final high-fidelity CFD/CSD simulation results

D2.12 Model validation and final report on TRIC concept (opens in new window)

Model validation and final report on TRIC concept

D2.28 Whirl tower test report (opens in new window)

Whirl tower test report

D3.16 Phase 3 Reporting (Minutes of checkpoint meeting, Activity report) (opens in new window)

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

D1.2 Report on analytical adaptive rotor studies (opens in new window)

Report on analytical adaptive rotor studies

D1.7 Refined blade design and morphing mechanism design targets (opens in new window)

Refined blade design and morphing mechanism design targets

D3.8 Phase 1 Reporting (Minutes of checkpoint meeting, Activity report) (opens in new window)

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

D1.15 Optimized morphed rotor blade shapes for low noise (opens in new window)

Optimized morphed rotor blade shapes for low noise

D2.32 Technology Compliance Matrix for morphing concepts (opens in new window)

Technology Compliance Matrix for morphing concepts

D3.9 Preliminary Design Review (PDR) (opens in new window)

Preliminary Design Review (PDR)

D2.3 Model validation and final report on SMA active twist (opens in new window)

Model validation and final report on SMA active twist

D2.27 Whirl tower test proof load requirements (opens in new window)

Whirl tower test proof load requirements

D1.11 Surrogate model of emissions versus rotor power required (opens in new window)

Surrogate model of emissions versus rotor power required

D2.4 Initial surrogate model of inertial twist and report (opens in new window)

Initial surrogate model of inertial twist and report

D2.17 Refined active tendon surrogate model (opens in new window)

Refined active tendon surrogate model

D2.14 Refined surrogate model of variable chord extension (opens in new window)

Refined surrogate model of variable chord extension

D2.2 Refined surrogate model of SMA active twist and report (opens in new window)

Refined surrogate model of SMA active twist and report

D2.13 Initial surrogate model of variable chord extension (opens in new window)

Initial surrogate model of variable chord extension

D2.5 Refined surrogate model of inertial twist and report (opens in new window)

Refined surrogate model of inertial twist and report

D2.10 Initial surrogate model of TRIC concept (opens in new window)

Initial surrogate model of TRIC concept

D2.11 Refined surrogate model of TRIC concept (opens in new window)

Refined surrogate model of TRIC concept

D2.1 Initial surrogate model of SMA active twist and report (opens in new window)

Initial surrogate model of SMA active twist and report

D1.10 Rotorcraft emissions model (opens in new window)

Rotorcraft emissions model

D2.16 Initial active tendon surrogate model (opens in new window)

Initial active tendon surrogate model

D1.8 Computed highly-resolved flow fields for T1.5 (opens in new window)

Computed highly-resolved flow fields for T1.5

D2.8 Refined surrogate model of FishBAC (opens in new window)

Refined surrogate model of FishBAC

D2.7 Initial surrogate model of FishBAC (opens in new window)

Initial surrogate model of FishBAC

D1.6 CFD/CSD coupled analysis running (opens in new window)

CFD/CSD coupled analysis running

D3.5 Intra consortium website set up for SABRE (opens in new window)

Intra consortium website set up for SABRE

D3.14 Special Session at AIAA Scitec Conference (opens in new window)

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 (opens in new window)

SABRE Project Handbook

D3.4 SABRE Project Overview Presentation (opens in new window)

SABRE Project Overview Presentation

D3.19 Final project booklet of results (opens in new window)

Final project booklet of results

D3.7 Project leaflet to identified stakeholders (opens in new window)

Project leaflet to identified stakeholders

D3.6 Public website, LinkedIn profile, and ResearchGate profile set up (opens in new window)

Public website, LinkedIn profile, and ResearchGate profile set up

Publications

Linearly variable chord-extension morphing for helicopter rotor blades (opens in new window)

Author(s): Rohin K. Majeti, Berend G. van der Wall, Christoph G. Balzarek
Published in: CEAS Aeronautical Journal, Issue 15 Oct 2020, 2020, Page(s) 00477-4, ISSN 1869-5582
Publisher: Springer Science + Business Media
DOI: 10.1007/s13272-020-00477-4

Passive energy balancing design for a linear actuated morphing wingtip structure (opens in new window)

Author(s): Jiaying Zhang, Chen Wang, Alexander D. Shaw, Mohammadreza Amoozgar, Michael I. Friswell
Published in: Aerospace Science and Technology, Issue 107, 2020, Page(s) 106279, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2020.106279

Aeroelastic model and analysis of an active camber morphing wing (opens in new window)

Author(s): Jiaying Zhang, Alexander D. Shaw, Chen Wang, Huaiyuan Gu, Mohammadreza Amoozgar, Michael I. Friswell, Benjamin K.S. Woods
Published in: Aerospace Science and Technology, Issue 111, 2021, Page(s) 106534, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2021.106534

Structural Modeling of Compliance-Based Camber Morphing Structures Under Transverse Shear Loading (opens in new window)

Author(s): Andres E. Rivero, Paul M. Weaver, Jonathan E. Cooper, Benjamin K. S. Woods
Published in: AIAA Journal, Issue 58/11, 2020, Page(s) 4941-4951, ISSN 0001-1452
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.J058842

Linearly variable chord-extension morphing for helicopter rotor blades (opens in new window)

Author(s): Rohin K. Majeti, Berend G. van der Wall, Christoph G. Balzarek
Published in: CEAS Aeronautical Journal, Issue 12/1, 2021, Page(s) 55-67, ISSN 1869-5582
Publisher: Springer Science + Business Media
DOI: 10.1007/s13272-020-00477-4

The effect of curved tips on the dynamics of composite rotor blades (opens in new window)

Author(s): M.R. Amoozgar, A.D. Shaw, M.I. Friswell
Published in: Aerospace Science and Technology, Issue 106, 2020, Page(s) 106197, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2020.106197

Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps (opens in new window)

Author(s): Andres E. Rivero, Stephane Fournier, Marinos Manolesos, Jonathan E. Cooper, Benjamin K. S. Woods
Published in: AIAA Journal, Issue Monthly, 2021, Page(s) 1-14, ISSN 0001-1452
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.j059606

Bidirectional torsional negative stiffness mechanism for energy balancing systems (opens in new window)

Author(s): Jiaying Zhang, Alexander D. Shaw, Mohammadreza Amoozgar, Michael I. Friswell, Benjamin K.S. Woods
Published in: Mechanism and Machine Theory, Issue 131, 2019, Page(s) 261-277, ISSN 0094-114X
Publisher: 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 (opens in new window)

Author(s): M.R. Amoozgar, A.D. Shaw, J. Zhang, M.I. Friswell
Published in: Journal of Fluids and Structures, Issue 87, 2019, Page(s) 124-136, ISSN 0889-9746
Publisher: 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 (opens in new window)

Author(s): M.R. Amoozgar, A.D. Shaw, J. Zhang, C. Wang, M.I. Friswell
Published in: Aerospace Science and Technology, Issue 91, 2019, Page(s) 539-547, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2019.05.053

Bidirectional Spiral Pulley Negative Stiffness Mechanism for Passive Energy Balancing (opens in new window)

Author(s): Jiaying Zhang, Alexander D. Shaw, Mohammadreza Amoozgar, Michael I. Friswell, Benjamin K. S. Woods
Published in: Journal of Mechanisms and Robotics, Issue 11/5, 2019, ISSN 1942-4302
Publisher: American Society of Mechanical Engineers
DOI: 10.1115/1.4043818

Composite Blade Twist Modification by Using a Moving Mass and Stiffness Tailoring (opens in new window)

Author(s): M. R. Amoozgar, A. D. Shaw, J. Zhang, M. I. Friswell
Published in: AIAA Journal, Issue 57/10, 2019, Page(s) 4218-4225, ISSN 0001-1452
Publisher: 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 (opens in new window)

Author(s): V. Ondra, B. Titurus
Published in: Journal of Sound and Vibration, Issue 461, 2019, Page(s) 114912, ISSN 0022-460X
Publisher: 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 (opens in new window)

Author(s): V. Ondra, B. Titurus
Published in: Thin-Walled Structures, Issue 144, 2019, Page(s) 106347, ISSN 0263-8231
Publisher: Elsevier BV
DOI: 10.1016/j.tws.2019.106347

Theoretical and experimental modal analysis of a beam-tendon system (opens in new window)

Author(s): V. Ondra, B. Titurus
Published in: Mechanical Systems and Signal Processing, Issue 132, 2019, Page(s) 55-71, ISSN 0888-3270
Publisher: Academic Press
DOI: 10.1016/j.ymssp.2019.06.016

Twist morphing of a composite rotor blade using a novel metamaterial (opens in new window)

Author(s): Huaiyuan Gu, Alexander D. Shaw, Mohammadreza Amoozgar, Jiaying Zhang, Chen Wang, Michael I. Friswell
Published in: Composite Structures, Issue 254, 2020, Page(s) 112855, ISSN 0263-8223
Publisher: Elsevier BV
DOI: 10.1016/j.compstruct.2020.112855

Modal analysis of a rotating pre-twisted beam axially loaded by an internally guided tendon (opens in new window)

Author(s): Jun Wu, Branislav Titurus
Published in: Journal of Sound and Vibration, Issue January 2021, 2021, Page(s) 115980, ISSN 0022-460X
Publisher: Academic Press
DOI: 10.1016/j.jsv.2021.115980

Effect of active camber morphing on rotor performance and control loads (opens in new window)

Author(s): Dominik Komp, Sumeet Kumar, Manfred Hajek, Jürgen Rauleder
Published in: Aerospace Science and Technology, Issue 108, 2021, Page(s) 106311, ISSN 1270-9638
Publisher: Elsevier BV
DOI: 10.1016/j.ast.2020.106311

A shape memory alloy torsion actuator for static blade twist (opens in new window)

Author(s): Salvatore Ameduri, Antonio Concilio
Published in: Journal of Intelligent Material Systems and Structures, Issue 30/17, 2019, Page(s) 2605-2626, ISSN 1045-389X
Publisher: SAGE Publications
DOI: 10.1177/1045389x19873396

Free vibration and stability analysis of a cantilever beam axially loaded by an intermittently attached tendon (opens in new window)

Author(s): V. Ondra, B. Titurus
Published in: Mechanical Systems and Signal Processing, Issue 158, 2021, Page(s) 107739, ISSN 0888-3270
Publisher: Academic Press
DOI: 10.1016/j.ymssp.2021.107739

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

Author(s): Kushagra Vidyarthi, Yasir Zahoor, Roeland De Breuker, Marilena Pavel, Mark Voskuijl
Published in: Proceedings of VFS International 76th Annual Forum, Issue 6-8 October 2020, 2020
Publisher: Vertical Flight Society

Manufacturing and characterisation of a composite FishBAC morphing wind tunnel model

Author(s): Andres E Rivero, Stephane Fournier, Paul Weaver, Jonathan Cooper, Benjamin King Sutton Woods
Published in: ICAST 2018: 29th International Conference on Adaptive Structures, Issue Annual, 2018, Page(s) 1-14
Publisher: International Conference on Adaptive Structures and Technologies

Effect of Active Camber on Rotor Noise, Power and Hub Vibration (opens in new window)

Author(s): Sumeet Kumar, Dominik Komp, Manfred Hajek, Juergen Rauleder
Published in: AIAA Scitech 2021 Forum, Issue January 2021, 2021, ISBN 978-1-62410-609-5
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2021-1927

Rotor Performance Enhancements with Spanwise Varying Active Camber Morphing (opens in new window)

Author(s): Dominik Komp, Manfred Hajek, Juergen Rauleder
Published in: AIAA Scitech 2021 Forum, Issue January 2021, 2021, ISBN 978-1-62410-609-5
Publisher: 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 (opens in new window)

Author(s): Antonio Concilio; Salvatore Ameduri; Bernardino Galasso; Antonio Gianvito
Published in: isbn: 9781510625853, Issue 1, 2019
Publisher: SPIE Digital Library
DOI: 10.1117/12.2511963

Shape memory alloys compact actuators for aerodynamic surfaces twisting (opens in new window)

Author(s): Salvatore Ameduri; Bernardino Galasso; Monica Ciminello; Antonio Concilio
Published in: AIAA Scitech 2020 Forum, Issue 3, 2020
Publisher: AIAA
DOI: 10.2514/6.2020-1299

Spiral Pulley Negative Stiffness Mechanism for Morphing Aircraft Actuation (opens in new window)

Author(s): Jiaying Zhang, Alexander D. Shaw, Amoozgar Mohammadreza, Michael I. Friswell, Benjamin K. S. Woods
Published in: Volume 5B: 42nd Mechanisms and Robotics Conference, Issue 26-29 August 2018, 2018, Page(s) V05BT07A003, ISBN 978-0-7918-5181-4
Publisher: ASME
DOI: 10.1115/DETC2018-85640

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

Author(s): MR Amoozgar, AD Shaw, J Zhang & MI Friswell
Published in: 6th Aircraft Structural Design Conference, Issue 9-11 October 2018, 2018
Publisher: Royal Aeronautical Society

Torsional Negative Stiffness Mechanism for Bidirectional Morphing Aircraft Actuation

Author(s): J Zhang, AD Shaw, MR Amoozgar, MI Friswell & BKS Woods
Published in: 6th Aircraft Structural Design Conference, Issue 9-11 October 2018, 2018
Publisher: Royal Aeronautical Society

Twist morphing of a hingeless rotor blade using a moving mass

Author(s): MR Amoozgar, AD Shaw, J Zhang & MI Friswell
Published in: 44th European Rotorcraft Forum, Issue 18-21 September 2018, 2018
Publisher: European Rotorcraft Forum

Static aeroelastic response of a rotor blade under internal axial loading

Author(s): R. Dibble, BKS Woods, B. Titurus
Published in: 43rd European Rotorcraft Forum, Issue 12-14 September 2017, 2017
Publisher: 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

Author(s): V. Ondra, R. Dibble, B. Titurus
Published in: 28th International Conference on Noise and Vibration engineering (ISMA2018), Issue 17 September 2018, 2018, ISBN 9789-073802995
Publisher: ISMA

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

Author(s): K. Vidyarthi, M. Beuker, F. Yin, M. Voskuijl, M. Pavel
Published in: 44th European Rotorcraft Forum, Issue 18-21 September 2018, 2018
Publisher: European Rotorcraft Forum

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

Author(s): R. K. Majeti, S. Benz
Published in: 8th Asian/Australian Rotorcraft Forum, Issue 30 Oct - 02 Nov 2019, 2019
Publisher: ARF

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

Author(s): S. Ameduri, A. Concilio, R K Majeti
Published in: ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Issue 9-11 September 2019, 2019
Publisher: American Society of Mechanical Engineers

Optimization of a Rotor with Morphing Blades using Particle Swarm Algorithm

Author(s): S. Benz, R. K. Majeti
Published in: Deutscher Luft und Raumfahrtkongress 2019, Issue 30 September - 2 October, 2019
Publisher: DGLR

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

Author(s): Majeti, Rohin Kumar und van der Wall, Berend G. und Balzarek, Christoph
Published in: Vertical Flight Society 75th Annual Forum, Issue 13.-16. May 2019, 2019
Publisher: VFS

Chord Morphing for Helicopter Rotor Blades (opens in new window)

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

Wind Tunnel Comparison of Flapped and FishBAC Camber Variation for Lift Control (opens in new window)

Author(s): Andres E. Rivero, Stephane Fournier, Marinos Manolesos, Jonathan E. Cooper, Benjamin Woods
Published in: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Publisher: 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 (opens in new window)

Author(s): Andres E. Rivero, Jonathan E. Cooper, Benjamin Woods
Published in: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Publisher: 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 (opens in new window)

Author(s): Stephane Fournier, Benjamin K. Woods
Published in: AIAA Scitech 2019 Forum, Issue Yearly, 2019, Page(s) 1-12, ISBN 978-1-62410-578-4
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1859

Structural Modelling of Compliance-Based Morphing Structures under Transverse Shear Loading (opens in new window)

Author(s): Andres E. Rivero, Paul Weaver, Benjamin K. Woods
Published in: AIAA Scitech 2019 Forum, Issue Yearly, 2019, Page(s) 1-17, ISBN 978-1-62410-578-4
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-0229

Tailored Nonlinear Negative Stiffness Mechanisms for Linear Motion

Author(s): J Zhang, AD Shaw, C Wang, MR Amoozgar, MI Friswell
Published in: IX ECCOMAS Thematic Conference on Smart Structures and Materials, Issue 8-12 June 2019, 2019, Page(s) 473-484, ISBN 978-84-949194-6-6
Publisher: International Centre for Numerical Methods in Engineering (CIMNE), Barcelona, Spain

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

Author(s): C Wang, J Zhang, AD Shaw, MR Amoozgar, MI Friswell, BKS Woods
Published in: IX ECCOMAS Thematic Conference on Smart Structures and Materials, Issue 8-12 July 2019, 2019, Page(s) 452-461, ISBN 978-84-949194-6-6
Publisher: International Centre for Numerical Methods in Engineering (CIMNE), Barcelona, Spain

Performance Analysis of Inertial Twist Morphing Concept in Hovering Flight

Author(s): MR Amoozgar, AD Shaw, J Zhang, C Wang, MI Friswell
Published in: 45th European Rotorcraft Forum 2019 (ERF), Issue 17-20 September 2019, 2019
Publisher: Warsaw Univeristy of Technology

Passive Energy Balancing for Morphing Rotorcraft Actuation: Integration and optimisation (opens in new window)

Author(s): Chen Wang, Jiaying Zhang, Mohammadreza Amoozgar, Alex Shaw, Michael Ian Friswell, Benjamin Woods
Published in: AIAA Scitech 2020 Forum, Issue 6-10 January 2020, 2020, Page(s) Paper AIAA 2020-1303, ISBN 978-1-62410-595-1
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1303

Aerodynamic Performance of Morphing Blades and Rotor Systems

Author(s): Rauleder, Jürgen; van der Wall, Berend G.; Woods, Benjamin K.S.; de Breuker, Roeland
Published in: AHS 74th Annual forum & Technology Display, Issue 14.-17. Mai 2018, 2018
Publisher: American Helicotper Society International

Integrated Rotor Performance Improvement and Vibration Reduction Using Active Camber Morphing (opens in new window)

Author(s): Sumeet Kumar, Dominik Komp, Manfred Hajek, Jürgen Rauleder
Published in: ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Issue 9-11 September 2019, 2019, ISBN 978-0-7918-5913-1
Publisher: 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 (opens in new window)

Author(s): Amine Abdelmoula, Stefan Platzer, Manfred Hajek, Juergen Rauleder
Published in: AIAA Scitech 2020 Forum, Issue 6-10 January 2020, 2020, ISBN 978-1-62410-595-1
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1302

Investigation of Active Rotor Design and Control for Performance Improvement

Author(s): Komp D, Kumar S, Abdelmoula A, Hajek M, Rauleder J.
Published in: Vertical Flight Society 75th Annual Forum & Technology DisplayAt: Philadelphia, Pennsylvania, Issue May 2019, 2019
Publisher: AHS International

Aerodynamic Performance of Morphed Camber Rotor Airfoils (opens in new window)

Author(s): Amine Abdelmoula, Juergen Rauleder
Published in: AIAA Scitech 2019 Forum, Issue 7-11 January 2019, 2019, ISBN 978-1-62410-578-4
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1101

Preliminary Design of a TE Morphing Surface for Rotorcraft (opens in new window)

Author(s): Yasir Zahoor, Roeland De Breuker, Mark Voskuijl
Published in: AIAA Scitech 2020 Forum, Issue January 2020, 2020, ISBN 978-1-62410-595-1
Publisher: 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

Author(s): Yasir Zahoor, Roeland De Breuker
Published in: Proceedings 2020 (Aerospace Europe Conference AEC2020, Issue 25-28 February 2020, 2020
Publisher: 3AF

The Aerodynamics of Active Camber (opens in new window)

Author(s): Benjamin King Sutton Woods
Published in: 28th ICAST conference, Issue 9-13 October 2017, 2017
Publisher: ICAST
DOI: 10.13140/rg.2.2.14104.70405

Aerodynamic Performance of Morphing Blades and Rotor Systems

Author(s): Juergen Rauleder; Van Der Wall, B. G.; Abdelmoula, A.; Komp, D.; Kumar, S.; Ondra, V.; Titurus, B.; Woods, B. K. S.
Published in: Scopus - Elsevier, Issue 1, 2018
Publisher: Elsevier

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