Kinetic comparative study on aerodynamic characteristics of hypersonic reentry vehicle from near-continuous flow to free molecular flow
Open Access
- 7 May 2021
- journal article
- research article
- Published by Springer Science and Business Media LLC in Advances in Aerodynamics
- Vol. 3 (1), 1-10
- https://doi.org/10.1186/s42774-021-00063-0
Abstract
No abstract availableKeywords
Other Versions
Funding Information
- National Numerical Wind Tunnel Project of China
This publication has 18 references indexed in Scilit:
- Progress and future prospects for particle-based simulation of hypersonic flowProgress in Aerospace Sciences, 2015
- Computer Modelling of Aerothermodynamic Characteristics for Hypersonic VehiclesJournal of Applied Mathematics and Physics, 2014
- A unified gas-kinetic scheme for continuum and rarefied flowsJournal of Computational Physics, 2010
- Particle and Continuum Method Comparison of a High-Altitude, Extreme-Mach-Number Reentry FlowJournal of Thermophysics and Heat Transfer, 2010
- Ab Initio Molecular DynamicsPublished by Cambridge University Press (CUP) ,2009
- Gas-kinetic numerical studies of three-dimensional complex flows on spacecraft re-entryJournal of Computational Physics, 2009
- Study on gas kinetic unified algorithm for flows from rarefied transition to continuumJournal of Computational Physics, 2004
- On the kinetic theory of rarefied gasesCommunications on Pure and Applied Mathematics, 1949
- Similarity Laws of Hypersonic FlowsJournal of Mathematics and Physics, 1946
- The General Law of Fall of a Small Spherical Body through a Gas, and its Bearing upon the Nature of Molecular Reflection from SurfacesPhysical Review B, 1923