The compressible Navier–Stokes equations are solved for turbulent spots in otherwise
laminar boundary layers with external flow Mach numbers of 3 and 6. In each case two wall …

Through high-resolution direct numerical simulations, the present study aims to investigate
several laminar-to-turbulent transition scenarios in the presence of wall heat transfer for …

Direct numerical simulations of supersonic boundary layers (SBLs) over a flat plate for M∞=
2.2 are performed for adiabatic and isothermal (cooled and heated) walls. Receptivity …

I. Introduction or high-speed aircraft, material and cooling issues for both airframe and
engine are one of the key elements which force the designer to limit the flight Mach number …

Direct numerical simulations (DNS) for supersonic boundary layers (SBLs) with a free-
stream Mach number of M∞= 2.2 are carried out. Various cases are investigated, involving …

This paper provides an insight into the optimisation of runtime and energy performance for
two widely-used CFD codes. Energy efficiency is a hot-topic in HPC and methods to reduce …

Abstract The Hartree Centre has been established as a UK focus for industrial engagement.
STFC has acquired a new IBM system based on the OpenPOWER architecture, comprising …

Direct numerical simulations (DNS) of both adiabatic and isothermal (heated and cooled)
supersonic boundary layers are performed. Two different transition scenarios, namely the …

I would like to acknowledge the access to French HPC resources provided by the French
regional computing center of Normandy CRIANN (1998022 and 2017002) and IDRIS (2017 …

Poster template: conference - A0 landscape (ppt) Page 1 Acknowledgement This work is part
of the Software Outlook program funded through a Service Level Agreement between STFC …