Abstract
Structural instabilities have traditionally been regarded as a failure mechanism; more recently, they have been
exploited as a means of designing shape adaptive structures. We are designing a passively actuated morphing
aerodynamic device which will utilise structural instabilities as a means of deploying. There are three main
requirements of this device; Firstly, it must exhibit large elastic deflections in response to small changes in a
controlling parameter. Secondly, the structure must not exhibit significant deflections until the controlling parameter
reaches a critical level. Finally, it must not undergo further shape change once it has traversed this large deflection
regime. In effect, this creates a ‘binary’ device, which is either fully stowed or fully deployed depending on the level
of the controlling parameter.
These needs are partially met by a structure with a snap-through instability, which exhibits a sudden shape change
when a limit point is reached. However, there will normally be significant deflections before this point, which violates
the second design requirement. A super-critical branching point structure is also only partially satisfactory; whilst
output deflections are initially small, out of plane deflections after the critical point occur gradually. Such structures
also rapidly re-stiffen, limiting the amount of possible shape change.
Taking a building-block approach, we combine structural components with different fundamental instabilities into a
morphing structure with the desired response. To aid the conceptual design of such a structure, we first explore
simple analytical bar-and-spring models with limited degrees of freedom. To achieve the desired response, the
output of one structure is connected to the input of a second—for example, the output deflection of a branching
point structure becomes the controlling parameter for a second structure with a snap-through response. The total
potential energy of the whole system is computed to identify the equilibrium paths and their stability.
Using these simple models, we demonstrate that structures which combine basic instabilities can be used to create
‘binary’ devices which meet our requirements. We show that these models can be used to capture the behaviour of
more complex structures which operate using the principle of combining instabilities. Future work will focus on using
such models as a tool for designing shape adaptive structures.
exploited as a means of designing shape adaptive structures. We are designing a passively actuated morphing
aerodynamic device which will utilise structural instabilities as a means of deploying. There are three main
requirements of this device; Firstly, it must exhibit large elastic deflections in response to small changes in a
controlling parameter. Secondly, the structure must not exhibit significant deflections until the controlling parameter
reaches a critical level. Finally, it must not undergo further shape change once it has traversed this large deflection
regime. In effect, this creates a ‘binary’ device, which is either fully stowed or fully deployed depending on the level
of the controlling parameter.
These needs are partially met by a structure with a snap-through instability, which exhibits a sudden shape change
when a limit point is reached. However, there will normally be significant deflections before this point, which violates
the second design requirement. A super-critical branching point structure is also only partially satisfactory; whilst
output deflections are initially small, out of plane deflections after the critical point occur gradually. Such structures
also rapidly re-stiffen, limiting the amount of possible shape change.
Taking a building-block approach, we combine structural components with different fundamental instabilities into a
morphing structure with the desired response. To aid the conceptual design of such a structure, we first explore
simple analytical bar-and-spring models with limited degrees of freedom. To achieve the desired response, the
output of one structure is connected to the input of a second—for example, the output deflection of a branching
point structure becomes the controlling parameter for a second structure with a snap-through response. The total
potential energy of the whole system is computed to identify the equilibrium paths and their stability.
Using these simple models, we demonstrate that structures which combine basic instabilities can be used to create
‘binary’ devices which meet our requirements. We show that these models can be used to capture the behaviour of
more complex structures which operate using the principle of combining instabilities. Future work will focus on using
such models as a tool for designing shape adaptive structures.
| Original language | English |
|---|---|
| Pages | 536-536 |
| Number of pages | 1 |
| Publication status | Published - 3 Jun 2022 |
| Event | ASCE Engineering Mechanics Institute Conference 2022 - Johns Hopkins University, Baltimore, United States Duration: 31 May 2022 → 3 Jun 2022 https://www.emi-conference.org/ |
Conference
| Conference | ASCE Engineering Mechanics Institute Conference 2022 |
|---|---|
| Abbreviated title | ASCE EMI 2022 |
| Country/Territory | United States |
| City | Baltimore |
| Period | 31/05/22 → 3/06/22 |
| Internet address |
Keywords
- nonlinear structures
- Path following
- stability
- buckling
- Mode interaction
- morphing structures
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Structural Function from Sequential, Interacting Elastic Instabilities
Wheatcroft, E., Shen, J., Groh, R., Pirrera, A. & Schenk, M., 26 Apr 2023, In: Proceedings of the Royal Society of London. Series A, Mathematical and Physical Sciences. 479, 2272, 20 p., 20220861.Research output: Contribution to journal › Article (Academic Journal) › peer-review
Open Access17 Citations (Scopus)3 Downloads (Pure) -
Conceptual Design of a Shape-Adaptive Structure With Tailored Structural Instability
Wheatcroft, E., Groh, R., Pirrera, A., Shen, J. & Schenk, M., 14 Nov 2022.Research output: Contribution to conference › Conference Paper › peer-review
2 Citations (Scopus)4 Downloads (Pure)
Student theses
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Design and Testing of a Passively-Actuated Spoiler for Gust Load Alleviation
Wheatcroft, E. D. (Author), Schenk, M. (Supervisor), Pirrera, A. (Supervisor) & Groh, R. (Supervisor), 30 Sept 2025Student thesis: Doctoral Thesis › Doctor of Philosophy (PhD)
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Prizes
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Royal Academy of Engineering Research Fellow
Groh, R. (Recipient), 2018
Prize: Prizes, Medals, Awards and Grants
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