Dr Philippe Lorrain

Research Associate
School of Engineering and Information Technology
+61 2 6268 8522

LOCATION

Building 16 Room 215 School of Engineering and Information Technology, The University of New South Wales, Australian Defence Force Academy, PO Box 7916, Canberra BC ACT 2610, AUSTRALIA

  • PUBLICATIONS

Journal articles

Lorrain P; Boyce R, 2011, 'Supersonic fin-body interactions in an internal scramjet flow', Journal of Propulsion and Power, vol. 27, pp. 319 - 329, 10.2514/1.49226

Conference Papers

Ogawa H; Capra B; Lorrain P, 2015, 'Numerical investigation of upstream fuel injection through porous media for scramjet engines via surrogate-assisted evolutionary algorithms', in 53rd AIAA Aerospace Sciences Meeting, presented at , 10.2514/6.2015-0884

Sopek T; Brieschenk S; Lorrain P; McIntyre TJ; Boyce RR, 2014, 'Code development to determine the temperature from the OH* chemiluminescence recordings in a supersonic combusting flow', in 45th AIAA Plasmadynamics and Lasers Conference, presented at

Brieschenk S; Lorrain P; Capra BR; Boyce RR; McIntyre TJ; Kleine H; O'Byrne S, 2012, 'Chemiluminescence imaging in supersonic combustors operating in radical-farming mode', in 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, presented at

Lorrain P; Brieschenk S; Capra BR; Boyce RR, 2012, 'A detailed investigation of nominally 2-D radical-farming scramjet combustion', in 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, presented at

Capra BR; Lorrain P; Boyce RR; Brieschenk S; Kuhn M; Hald H, 2012, 'H2- O2porous fuel injection in a radical farming scramjet', in 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, presented at

Lorrain P; Boyce R; Omlor B, 2009, '3-D influences on nominally 2-D strut injection supersonic combustion', in 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, presented at