Shock-stable flux scheme for predicting aerodynamic heating load of hypersonic airliners
- 27 March 2019
- journal article
- research article
- Published by Springer Science and Business Media LLC in Science China Physics Mechanics and Astronomy
- Vol. 62 (8), 984711
- https://doi.org/10.1007/s11433-018-9347-6
Abstract
No abstract availableKeywords
This publication has 30 references indexed in Scilit:
- Carbuncle Phenomena and Other Shock Anomalies in Three DimensionsAIAA Journal, 2012
- Parameter-Free Simple Low-Dissipation AUSM-Family Scheme for All SpeedsAIAA Journal, 2011
- An improved low diffusion E-CUSP upwind schemeComputers & Fluids, 2011
- Evaluation of Euler Fluxes for Hypersonic Heating ComputationsAIAA Journal, 2010
- Cures for the shock instability: Development of a shock-stable Roe schemeJournal of Computational Physics, 2003
- Mass Flux Schemes and Connection to Shock InstabilityJournal of Computational Physics, 2000
- Two-equation eddy-viscosity turbulence models for engineering applicationsAIAA Journal, 1994
- On Godunov-type methods near low densitiesJournal of Computational Physics, 1991
- Attempt to Evaluate the Computations for Test Case 6.1 - Cold Hypersonic Flow Past Ellipsoidal Shapes -Published by Springer Science and Business Media LLC ,1991
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981