The complexity and mechanism of transonic aeroelastic problems Article Swipe
Weiwei Zhang
,
Chuanqiang Gao
,
Zhengyin Ye
·
YOU?
·
· 2018
· Open Access
·
· DOI: https://doi.org/10.1360/n972018-00151
YOU?
·
· 2018
· Open Access
·
· DOI: https://doi.org/10.1360/n972018-00151
In high-speed flight, transonic aeroelasticity commonly exists, leading to various problems such as transonic flutter, buffeting and buzz. To solve these problems, a good understanding of the underlying physical mechanisms is critical. Unfortunately, the nonlinearity and unsteadiness of airflows complicate this process and consequently impede the development of aircraft design. Here using the numerical simulation and modeling of complex transonic flows, we developed a unified analytical method for aeroelastic stability and response problems. We then explored the mechanisms of three complex aeroelastic phenomena and unveiled their relationships. (1) Transonic buzz is in essence a single degree of freedom (SDOF) flutter caused by the coupling between the most unstable fluid mode and structural mode. SDOF flutter of this kind is possible only when the fluid exhibits sufficiently low damping; that is, the freestream flow is near the buffet boundary or in the low supersonic zone. Besides, the unstable frequency boundaries are determined by zero and pole of the open loop system. (2) The frequency lock-in phenomenon in the transonic buffeting flow is caused by the SDOF flutter in the unstably separated flow rather than resonance. In this process, the response undergoes a transition from the forced vibration to the self-excited flutter, which results in a deviation of the lock-in region from the resonance point. By contrast, the traditional uncoupled method misestimates the risk range and underestimates the amplitude of a vibration. (3) When the pitching degree of freedom is released, transonic buffet will be induced at a lower angle of attack, indicative of the drawbacks of predicting buffet onset by a rigid model. Actually, the elastic characteristic plays a key role in predicting buffet onset in aircraft design. Collectively, the large-amplitude structural vibration in the transonic flow is closely related to aeroelastic instability. The dynamic linear model can correctly predict the boundary of some complex dynamic phenomena. The complexity of transonic aeroelasticity mainly arises from the stability reduction of airflows. Different from classical aeroelastic problems, the new fluid mode is derived from the reduction of fluid stability. The coupling between such a fluid mode and structural mode often leads to complex phenomena in transonic flows.
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- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1360/n972018-00151
- http://engine.scichina.com/doi/pdf/adbb6a9547ee48a2b17f59b2c06886e3
- OA Status
- bronze
- Cited By
- 2
- References
- 32
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W2800143180
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W2800143180Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.1360/n972018-00151Digital Object Identifier
- Title
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The complexity and mechanism of transonic aeroelastic problemsWork title
- Type
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articleOpenAlex work type
- Language
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enPrimary language
- Publication year
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2018Year of publication
- Publication date
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2018-03-19Full publication date if available
- Authors
-
Weiwei Zhang, Chuanqiang Gao, Zhengyin YeList of authors in order
- Landing page
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https://doi.org/10.1360/n972018-00151Publisher landing page
- PDF URL
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https://engine.scichina.com/doi/pdf/adbb6a9547ee48a2b17f59b2c06886e3Direct link to full text PDF
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YesWhether a free full text is available
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bronzeOpen access status per OpenAlex
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https://engine.scichina.com/doi/pdf/adbb6a9547ee48a2b17f59b2c06886e3Direct OA link when available
- Concepts
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Aeroelasticity, Transonic, Mechanism (biology), Computer science, Structural engineering, Aerodynamics, Engineering, Aerospace engineering, Philosophy, EpistemologyTop concepts (fields/topics) attached by OpenAlex
- Cited by
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2Total citation count in OpenAlex
- Citations by year (recent)
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2024: 1, 2018: 1Per-year citation counts (last 5 years)
- References (count)
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32Number of works referenced by this work
- Related works (count)
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10Other works algorithmically related by OpenAlex
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| abstract_inverted_index.results | 201 |
| abstract_inverted_index.system. | 159 |
| abstract_inverted_index.unified | 64 |
| abstract_inverted_index.various | 9 |
| abstract_inverted_index.Besides, | 144 |
| abstract_inverted_index.aircraft | 48, 275 |
| abstract_inverted_index.airflows | 38 |
| abstract_inverted_index.boundary | 137, 300 |
| abstract_inverted_index.commonly | 5 |
| abstract_inverted_index.coupling | 103, 337 |
| abstract_inverted_index.damping; | 127 |
| abstract_inverted_index.exhibits | 124 |
| abstract_inverted_index.explored | 75 |
| abstract_inverted_index.flutter, | 14, 199 |
| abstract_inverted_index.modeling | 56 |
| abstract_inverted_index.physical | 28 |
| abstract_inverted_index.pitching | 233 |
| abstract_inverted_index.possible | 119 |
| abstract_inverted_index.problems | 10 |
| abstract_inverted_index.process, | 186 |
| abstract_inverted_index.response | 71, 188 |
| abstract_inverted_index.unstable | 107, 146 |
| abstract_inverted_index.unstably | 178 |
| abstract_inverted_index.unveiled | 84 |
| abstract_inverted_index.Actually, | 262 |
| abstract_inverted_index.Different | 319 |
| abstract_inverted_index.Transonic | 88 |
| abstract_inverted_index.airflows. | 318 |
| abstract_inverted_index.amplitude | 226 |
| abstract_inverted_index.buffeting | 15, 168 |
| abstract_inverted_index.classical | 321 |
| abstract_inverted_index.contrast, | 214 |
| abstract_inverted_index.correctly | 297 |
| abstract_inverted_index.critical. | 31 |
| abstract_inverted_index.developed | 62 |
| abstract_inverted_index.deviation | 204 |
| abstract_inverted_index.drawbacks | 253 |
| abstract_inverted_index.frequency | 147, 162 |
| abstract_inverted_index.numerical | 53 |
| abstract_inverted_index.phenomena | 82, 350 |
| abstract_inverted_index.problems, | 21, 323 |
| abstract_inverted_index.problems. | 72 |
| abstract_inverted_index.reduction | 316, 332 |
| abstract_inverted_index.released, | 238 |
| abstract_inverted_index.resonance | 211 |
| abstract_inverted_index.separated | 179 |
| abstract_inverted_index.stability | 69, 315 |
| abstract_inverted_index.transonic | 3, 13, 59, 167, 239, 284, 309, 352 |
| abstract_inverted_index.uncoupled | 217 |
| abstract_inverted_index.undergoes | 189 |
| abstract_inverted_index.vibration | 195, 281 |
| abstract_inverted_index.analytical | 65 |
| abstract_inverted_index.boundaries | 148 |
| abstract_inverted_index.complexity | 307 |
| abstract_inverted_index.complicate | 39 |
| abstract_inverted_index.determined | 150 |
| abstract_inverted_index.freestream | 131 |
| abstract_inverted_index.high-speed | 1 |
| abstract_inverted_index.indicative | 250 |
| abstract_inverted_index.mechanisms | 29, 77 |
| abstract_inverted_index.phenomena. | 305 |
| abstract_inverted_index.phenomenon | 164 |
| abstract_inverted_index.predicting | 255, 271 |
| abstract_inverted_index.resonance. | 183 |
| abstract_inverted_index.simulation | 54 |
| abstract_inverted_index.stability. | 335 |
| abstract_inverted_index.structural | 111, 280, 344 |
| abstract_inverted_index.supersonic | 142 |
| abstract_inverted_index.transition | 191 |
| abstract_inverted_index.underlying | 27 |
| abstract_inverted_index.vibration. | 229 |
| abstract_inverted_index.aeroelastic | 68, 81, 290, 322 |
| abstract_inverted_index.development | 46 |
| abstract_inverted_index.traditional | 216 |
| abstract_inverted_index.consequently | 43 |
| abstract_inverted_index.instability. | 291 |
| abstract_inverted_index.misestimates | 219 |
| abstract_inverted_index.nonlinearity | 34 |
| abstract_inverted_index.self-excited | 198 |
| abstract_inverted_index.sufficiently | 125 |
| abstract_inverted_index.unsteadiness | 36 |
| abstract_inverted_index.Collectively, | 277 |
| abstract_inverted_index.understanding | 24 |
| abstract_inverted_index.Unfortunately, | 32 |
| abstract_inverted_index.aeroelasticity | 4, 310 |
| abstract_inverted_index.characteristic | 265 |
| abstract_inverted_index.relationships. | 86 |
| abstract_inverted_index.underestimates | 224 |
| abstract_inverted_index.large-amplitude | 279 |
| cited_by_percentile_year.max | 94 |
| cited_by_percentile_year.min | 90 |
| countries_distinct_count | 0 |
| institutions_distinct_count | 3 |
| citation_normalized_percentile.value | 0.48772278 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |