A High-Order Continuum Model for Computational Hypersonic Aerodynamics

Reese, Jason (Principal Investigator)

Mechanical And Aerospace Engineering

Project: Research

Project Details

Status	Finished
Effective start/end date	1/09/04 → 30/09/07

Funding

EPSRC (Engineering and Physical Sciences Research Council): £134,269.00

3 Article
2 Paper
1 Conference contribution book
1 Speech

A parallel compact-TVD method for compressible fluid dynamics employing shared and distributed-memory paradigms
Fico, V., Emerson, D. & Reese, J., Jun 2011, In : Computers and Fluids. 45, 1, p. 172-176 5 p.
Research output: Contribution to journal › Article

File
5 Citations (Scopus)

151 Downloads (Pure)
Implementation of semi-discrete, non-staggered central schemes in a collated, polyhedral, finite volume framework, for high-speed viscous flows
Greenshields, C. J., Weller, H. G., Gasparini, F. & Reese, J. M., 10 May 2010, In : International Journal of Numerical Methods for Heat and Fluid Flow. 63, p. 1-21 21 p.
Research output: Contribution to journal › Article
240 Citations (Scopus)

77 Downloads (Pure)
The structure of hypersonic shock waves using Navier-Stokes equations modified to include mass diffusion
Greenshields, C. J. & Reese, J. M., Jul 2007, 2nd European Conference on Aero-Space Sciences (EUCASS). 8 p.
Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

Open Access
File
67 Downloads (Pure)