Stagnation point heat flux characterization under numerical error and boundary conditions uncertainty
DOI10.1016/J.EUROMECHFLU.2022.05.005zbMath1495.76072OpenAlexW4280499254WikidataQ113874303 ScholiaQ113874303MaRDI QIDQ2163021
Pietro Marco Congedo, Andrea F. Cortesi, Thierry E. Magin, Michele Capriati
Publication date: 9 August 2022
Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.euromechflu.2022.05.005
uncertainty quantificationsurrogate modelatmospheric entry flowschemically reacting Navier-Stokes equationsmodified Steger-Warming MUSCL schemethree-dimensional finite volume solver
Finite volume methods applied to problems in fluid mechanics (76M12) Stochastic analysis applied to problems in fluid mechanics (76M35) Reaction effects in flows (76V05) Hypersonic flows (76K05) Diffusive and convective heat and mass transfer, heat flow (80A19)
Uses Software
Cites Work
- Unnamed Item
- A procedure for the estimation of the numerical uncertainty of CFD calculations based on grid refinement studies
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
- Mutation++
- Efficient uncertainty quantification of stochastic CFD problems using sparse polynomial chaos and compressed sensing
- Current grid generation strategies and future requirements in hypersonic vehicle design, analysis and testing
- A BGK model for high temperature rarefied gas flows
- Numerical investigation of a hypersonic flow around a capsule in \(\mathrm{CO}_2\)-\(\mathrm{N}_2\) environment
- Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
- An unstructured, three-dimensional, shock-fitting solver for hypersonic flows
- Exploiting active subspaces to quantify uncertainty in the numerical simulation of the hyshot II scramjet
- A Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output from a Computer Code
- Aerothermodynamics – A critical review at DLR
- On the distribution of points in a cube and the approximate evaluation of integrals
- US3D
This page was built for publication: Stagnation point heat flux characterization under numerical error and boundary conditions uncertainty
