Verification and Validation Issues in Hypersonic Stability and Transition Prediction
The development, validation, and introduction of physics-based approaches for stability and transition prediction will lead to smaller and more manageable uncertainties in the design of hypersonic vehicles. Through mechanism identification, verification, and validation activities for two- and three-...
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Veröffentlicht in: | Journal of spacecraft and rockets 2015-01, Vol.52 (1), p.29-37 |
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Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | The development, validation, and introduction of physics-based approaches for stability and transition prediction will lead to smaller and more manageable uncertainties in the design of hypersonic vehicles. Through mechanism identification, verification, and validation activities for two- and three-dimensional geometries, the following have been learned in applying stability formulations: 1) Related to verification of the basic state, the acid test is to refine the basic state until the stability results do not change; 2) A good verification test for the stability formulation is to be sure the linear problem is correctly modeled; 3) In validation, it is very important to work on the same geometries computationally and experimentally and confirm them; for example, model alignment and freestream flow angularity are found to be important; 4) From verification studies on three-dimensional geometries, numerical errors, especially near the windward plane, can seed the stationary crossflow instability in the supposedly undisturbed basic state; the stationary crossflow instability is sensitive; 5) The marching path is important for three-dimensional geometries and should be in the group-velocity direction; the N factor has some uncertainty in it, and caution should be used in quoting it with precision; and 6) Nonlinear effects should be included in detailed studies of crossflow instability necessitating a nonlinear parabolized stability equation or direct numerical simulation approach. |
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ISSN: | 0022-4650 1533-6794 |
DOI: | 10.2514/1.A32825 |