Flow characterisation of transpiring porous media for hypersonic vehicles

Conference item

This paper experimentally examines the internal and external flow characteristics of porous zirconium diboride (Z rB2), an Ultra-High-Temperature-Ceramic (UHTC) and a potential candidate for transpiration cooling of hypersonic vehicles. This is performed for both partially sintered material and fully densified material with cast features. The Darcy and Forchheimer permeability coefficients of these samples are determined using an ISO standard test rig. The outflow of the transpiring porous samples is investigated where no hypersonic cross-flow is involved using hot-wire anemometry and focused Schlieren visualisation. The velocity maps obtained from the hot-wire data show significant non-uniformities across the UHTC’s outflow region, both at low and high differential pressures. The focused Schlieren using carbon dioxide as the injected gas reveals unsteady structures at high differential pressures as the outflowing gas interacts with the surrounding air.

Authors: Ifti, H; Hermann, T; McGilvray, M

• Publication status: Published
• Peer review status: Peer reviewed
• Publisher: American Institute of Aeronautics and Astronautics
• Host title: 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, AIAA SPACE Forum, (AIAA 2018-5167)
• Journal: 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
• Publication date: 2018-09-17
• Acceptance date: 2018-04-08
• DOI: 10.2514/6.2018-5167
• ISBN: 9781624105777