Structural Admissibility and Material-Driven Stability in Hypersonic Flight
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| Formato: | Recurso digital |
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2026
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| _version_ | 1866901102894514176 |
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| author | Lumenis IO PTY LTD |
| author_facet | Lumenis IO PTY LTD |
| contents | <p>This research program investigates the fundamental conditions under which sustained hypersonic flight is physically and structurally admissible. Rather than optimizing specific vehicles, configurations, or material compositions, the work adopts a constraint-based, model-agnostic framework designed to identify necessary conditions for stability in extreme flow regimes. Classical assumptions embedded in predefined turbulence models, fixed material properties, empirical heat-transfer laws, and control-centric design methodologies are explicitly excluded. Across multiple studies, hypersonic flight is reframed as a materials-driven, co-evolutionary systems problem in which stability emerges only through coupled interaction between flow, geometry, and material response. This approach challenges long-standing assumptions of passive material endurance and control-dominated stability, offering a structural explanation for persistent experimental difficulties observed in hypersonic programs.</p> |
| format | Recurso digital |
| id | zenodo_https___doi_org_10_5281_zenodo_18521264 |
| institution | Zenodo |
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| publishDate | 2026 |
| publisher | Zenodo |
| record_format | zenodo |
| spellingShingle | Structural Admissibility and Material-Driven Stability in Hypersonic Flight Lumenis IO PTY LTD Hypersonic flight Structural admissibility Constraint-based modeling Model-agnostic simulation Nonlinear stability Extreme flow regimes Flow–structure interaction Co-evolutionary dynamics Hypersonic instability Systems-level analysis <p>This research program investigates the fundamental conditions under which sustained hypersonic flight is physically and structurally admissible. Rather than optimizing specific vehicles, configurations, or material compositions, the work adopts a constraint-based, model-agnostic framework designed to identify necessary conditions for stability in extreme flow regimes. Classical assumptions embedded in predefined turbulence models, fixed material properties, empirical heat-transfer laws, and control-centric design methodologies are explicitly excluded. Across multiple studies, hypersonic flight is reframed as a materials-driven, co-evolutionary systems problem in which stability emerges only through coupled interaction between flow, geometry, and material response. This approach challenges long-standing assumptions of passive material endurance and control-dominated stability, offering a structural explanation for persistent experimental difficulties observed in hypersonic programs.</p> |
| title | Structural Admissibility and Material-Driven Stability in Hypersonic Flight |
| topic | Hypersonic flight Structural admissibility Constraint-based modeling Model-agnostic simulation Nonlinear stability Extreme flow regimes Flow–structure interaction Co-evolutionary dynamics Hypersonic instability Systems-level analysis |
| url | https://doi.org/10.5281/zenodo.18521264 |