Morphing Wing Droop Nose with Large Deformation: Ground Tests and Lessons Learned Article Swipe
Srinivas Vasista
,
Johannes Riemenschneider
,
Ralf Keimer
,
Hans Peter Monner
,
Felix Nolte
,
Peter Horst
·
YOU?
·
· 2019
· Open Access
·
· DOI: https://doi.org/10.3390/aerospace6100111
YOU?
·
· 2019
· Open Access
·
· DOI: https://doi.org/10.3390/aerospace6100111
A design for a new high lift system that features a morphing wing leading edge “droop nose” has the potential to generate high lift coefficients whilst mitigating airframe noise emissions. This seamless, continuous, and stepless flexible droop nose potentially offers improvements to stall and compressor requirements for an internally-blown active Coandă trailing edge flap. A full-scale, span-trimmed three-dimensional droop nose was manufactured and ground-tested based on results obtained from new design synthesis tools. A new component of the droop nose is the hybrid fiberglass-elastomeric skin that is tailored in stiffness to meet morphing curvature requirements and spanwise bending resistance. A manufacturing concept of the novel skin was established that led to an adequate manufacturing quality. The skin was driven and supported by two optimized kinematic ribs and conventional actuators and overall shape results show good agreement apart from the region closest to the leading edge. Kinematic trajectory measurements showed that the kinematics met the target trajectories well, with and without the influence of the skin, and it was deemed that the error in curvature is due to a higher than expected skin stiffness in the hybrid layer. Calculated actuator torque levels and strain measurements corroborate this inference. The lessons learned show that means of adjustment post-assembly are needed, and a reduction of torque, energy and a better curvature distribution may be achieved if the skin at the spar junction is allowed to move relative to the main wing. Careful aerodynamic, structural, actuation and manufacturing trade-off studies would be needed to determine the overall performance benefit.
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Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.3390/aerospace6100111
- https://www.mdpi.com/2226-4310/6/10/111/pdf
- OA Status
- gold
- Cited By
- 16
- References
- 35
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W2978335629
All OpenAlex metadata
Raw OpenAlex JSON
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https://openalex.org/W2978335629Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.3390/aerospace6100111Digital Object Identifier
- Title
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Morphing Wing Droop Nose with Large Deformation: Ground Tests and Lessons LearnedWork title
- Type
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articleOpenAlex work type
- Language
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enPrimary language
- Publication year
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2019Year of publication
- Publication date
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2019-10-02Full publication date if available
- Authors
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Srinivas Vasista, Johannes Riemenschneider, Ralf Keimer, Hans Peter Monner, Felix Nolte, Peter HorstList of authors in order
- Landing page
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https://doi.org/10.3390/aerospace6100111Publisher landing page
- PDF URL
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https://www.mdpi.com/2226-4310/6/10/111/pdfDirect link to full text PDF
- Open access
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YesWhether a free full text is available
- OA status
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goldOpen access status per OpenAlex
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https://www.mdpi.com/2226-4310/6/10/111/pdfDirect OA link when available
- Concepts
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Structural engineering, Engineering, Voltage droop, Airfoil, Wing, Mechanical engineering, Electrical engineering, Voltage divider, VoltageTop concepts (fields/topics) attached by OpenAlex
- Cited by
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16Total citation count in OpenAlex
- Citations by year (recent)
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2025: 1, 2024: 3, 2023: 2, 2022: 4, 2021: 2Per-year citation counts (last 5 years)
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35Number of works referenced by this work
- Related works (count)
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10Other works algorithmically related by OpenAlex
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