Composite Blade Twist Modification by Using a Moving Mass and Stiffness Tailoring
- Submitting institution
-
The University of Huddersfield
- Unit of assessment
- 12 - Engineering
- Output identifier
- 57
- Type
- D - Journal article
- DOI
-
10.2514/1.J057591
- Title of journal
- AIAA Journal
- Article number
- -
- First page
- 4218
- Volume
- 57
- Issue
- 10
- ISSN
- 0001-1452
- Open access status
- Technical exception
- Month of publication
- January
- Year of publication
- 2019
- URL
-
-
- Supplementary information
-
-
- Request cross-referral to
- -
- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
-
3
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- This paper proposes new morphing concept for composite helicopter blades. The study was funded by the Horizon 2020 Program project “Shape adaptive blades for rotorcraft efficacy” (grant agreement 723491). Amoozgar who was a post doctoral researcher on this project has continued collaboration with Swansea University in the EPSRC programme grant EP/R006768/1. As a direct result of this study, Amoozgar was appointed as a senior lecture in Mechanical Engineering at University of Huddersfield. Also, this study resulted in initiation of a new collaboration with Bristol University J.E.copper@bristol.ac.uk and Khalifa University rafic.ajaj@ku.ac.ae working on the dynamics and aeroelasticity of morphing aircraft.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -
