2015
DOI: 10.1016/j.jcp.2015.09.001
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Exploiting active subspaces to quantify uncertainty in the numerical simulation of the HyShot II scramjet

Abstract: We present a computational analysis of the reactive flow in a hypersonic scramjet engine with focus on effects of uncertainties in the operating conditions. We employ a novel methodology based on active subspaces to characterize the effects of the input uncertainty on the scramjet performance. The active subspace identifies one-dimensional structure in the map from simulation inputs to quantity of interest that allows us to reparameterize the operating conditions; instead of seven physical parameters, we can u… Show more

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Cited by 135 publications
(91 citation statements)
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“…Nevertheless a wide range of functions of interest in engineering applications present an active subspace of dimension one or two, resulting in a great reduction of the parameter space. Among others we cite shape optimization [23], and uncertainty quantification in the numerical simulation of the HyShot II screamjet [10]. We would also like to mention some naval engineering applications of the active subspaces: coupled with boundary element method and free form deformation [41], for propeller blade design [24], and a shared subspace application for constraint optimisation [38].…”
Section: Active Subspaces For Modal Coefficient Reconstructionmentioning
confidence: 99%
“…Nevertheless a wide range of functions of interest in engineering applications present an active subspace of dimension one or two, resulting in a great reduction of the parameter space. Among others we cite shape optimization [23], and uncertainty quantification in the numerical simulation of the HyShot II screamjet [10]. We would also like to mention some naval engineering applications of the active subspaces: coupled with boundary element method and free form deformation [41], for propeller blade design [24], and a shared subspace application for constraint optimisation [38].…”
Section: Active Subspaces For Modal Coefficient Reconstructionmentioning
confidence: 99%
“…If the points in the scatter plot reveal a univariate or near univariate relationship, then the ridge approximation Equation 6 with W 1 = w is a good approximation to f (x). If the points in the scatter plot do not reveal a functional relationship, then the model Equation 6 with W 1 = w may not be appropriate.…”
Section: Validating Important Directions With Summary Plotsmentioning
confidence: 99%
“…trailing edge half-thickness x 7 wedge angle x 8 wedge half-angle x 9 upper surface inflection x 10 lower surface inflection x 11 leading edge radius…”
Section: Iid Parsec Airfoilsmentioning
confidence: 99%