Estimation of inflow uncertainties in laminar hypersonic double-cone experiments

J. Ray, I. Nompelis, G. V. Candler, S. Kieweg, D. Dinzl, B. Carnes, V. G. Weirs, B. Freno, M. Howard, T. Smith

Research output: Contribution to journalArticlepeer-review

19 Scopus citations

Abstract

This paper proposes a probabilistic framework for assessing the consistency of an experimental dataset, i.e., whether the stated experimental conditions are consistent with the measurements provided. In case the dataset is inconsistent, our framework allows one to hypothesize and test sources of inconsistencies. This is crucial in model validation efforts. The framework relies on Bayesian inference to estimate experimental settings deemed uncertain, from measurements deemed accurate. The quality of the inferred variables is gauged by its ability to reproduce held-out experimental measurements. The correctness of the framework is tested on three double-cone experiments conducted in the Calspan-University at Buffalo Research Center’s Large Energy National Shock Tunnel-I (LENS-I), which have also been numerically simulated successfully. Thereafter, the framework is used to investigate two double-cone experiments (executed in the LENS-XX), which have encountered difficulties when used in model validation exercises. An inconsistency is detected with one of the LENS-XX experiments. In addition, two causes are hypothesized for our inability to simulate LEXS-XX experiments accurately and are tested using our framework. It is found that there is no single cause that explains all the discrepancies between model predictions and experimental data, but different causes explain different discrepancies, to larger or smaller extent. This paper proposes that uncertainty quantification methods be used more widely to understand experiments and characterize facilities, and three different methods are cited to do so, the third of which is presented in this paper.

Original languageEnglish (US)
Pages (from-to)4461-4474
Number of pages14
JournalAIAA journal
Volume58
Issue number10
DOIs
StatePublished - 2020

Bibliographical note

Publisher Copyright:
© 2020 by the American Institute of Aeronautics and Astronautics, Inc.

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