📣 Help Shape the Future of UKRI's Gateway to Research (GtR)

We're improving UKRI's Gateway to Research and are seeking your input! If you would be interested in being interviewed about the improvements we're making and to have your say about how we can make GtR more user-friendly, impactful, and effective for the Research and Innovation community, please email gateway@ukri.org.

Parallel multiscale simulation of hypersonic flow with porous wall injection

First Author: Cerminara A

Attributed to: Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.4203/ccp.112.11

Publication URI: http://dx.doi.org/10.4203/ccp.112.11

Type: Conference/Paper/Proceeding/Abstract