Hypersonic International Flight Research Experimentation Flight 2 Unstart Reliability Analysis

The objective of this work was to assess the unstart reliability of the Hypersonic International Flight Research Experimentation Flight 2 system. To do this, a quantification of margins and uncertainties framework was used for comparing the predicted combustion-induced shock location to the predicte...

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Veröffentlicht in:	Journal of propulsion and power 2024-03, Vol.40 (2), p.169-180
Hauptverfasser:	West, Thomas K., Bynum, Michael D.
Format:	Artikel
Sprache:	eng
Schlagworte:	Computational fluid dynamics Errors Experimentation Experiments Flight conditions Flight vehicles Fluid dynamics Fluid flow Polynomials Random variables Reliability analysis Statistical analysis Uncertainty Verification Viscosity
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