Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Rowan Gollan"'
Publikováno v:
AIAA Journal. 60:2798-2809
This paper presents a correlation to obtain the surface species concentration on a stagnation point with mass injection for hypersonic flow. The correlation can be used to determine surface recombination heat fluxes and oxidation levels for ablatives
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Jamie Border, Rowan Gollan
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
This paper presents numerical results investigating the aerodynamic and aerothermal effects of mass injection applied to hypersonic sharp leading edges, in the context of active thermal protection systems. A numerical study was carried out using Eilm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::60e8e7131aa634b86be438af6913f59b
https://ora.ox.ac.uk/objects/uuid:774fc566-5f71-4cb8-8e7f-bc8b9c0af269
https://ora.ox.ac.uk/objects/uuid:774fc566-5f71-4cb8-8e7f-bc8b9c0af269
Autor:
Alexis Lefevre, David Gildfind, Rowan Gollan, Peter Jacobs, Timothy McIntyre, Christopher M. James
Publikováno v:
AIAA SCITECH 2022 Forum.
Autor:
Rowan Gollan
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withstand severe thermal loads. Heating to the vehicle surface arises as convective, catalytic and radiative heat flux due to the high temperature of the sho
Externí odkaz:
http://espace.library.uq.edu.au/view/UQ:178818
Autor:
Rowan Gollan
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withstand severe thermal loads. Heating to the vehicle surface arises as convective, catalytic and radiative heat flux due to the high temperature of the sho
Externí odkaz:
http://espace.library.uq.edu.au/view/UQ:178818