Items where Author is "Sandham, Neil"
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Number of items: 8.
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CERMINARA, Adriano, DURANT, Antoine, ANDRÉ, Thierry, SANDHAM, Neil and TAYLOR, Nigel J.
(2018).
DNS of acoustic receptivity and breakdown in a Mach 6 flow over a generic forebody.
In: 2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida, 08–12 January 2018.
American Institute of Aeronautics and Astronautics.
CERMINARA, Adriano and SANDHAM, Neil
(2016).
Boundary-layer receptivity and breakdown in hypersonic flow over a swept blunt wedge with three-dimensional freestream acoustic disturbances.
In: 8th AIAA Flow Control Conference, Washington, D.C., 13-17 June 2016.
American Institute of Aeronautics and Astronautics.
KONTOGIANNIS, Konstantinos, CERMINARA, Adriano, TAYLOR, Nigel J., SOBESTER, Andras and SANDHAM, Neil
(2015).
Parametric geometry models for hypersonic aircraft components: blunt leading edges.
In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
American Institute of Aeronautics and Astronautics.
CERMINARA, Adriano and SANDHAM, Neil
(2015).
Leading-edge receptivity to acoustic waves for high-speed flows over a blunt wedge.
In: 45th AIAA Fluid Dynamics Conference, Dallas, TX, 22-26 Jun 2015.
American Institute of Aeronautics and Astronautics.
Public
SHARMA, Pushpender, DEITERDING, Ralph, CERMINARA, Adriano and SANDHAM, Neil
(2023).
Numerical simulation of transpiration cooling for a high-speed boundary layer undergoing transition to turbulence.
Aerospace Science and Technology, 141: 108581.
CERMINARA, Adriano, HERMANN, Tobias, IFTI, Hassan Saad, DEITERDING, Ralf, SANDHAM, Neil and MCGILVRAY, Matthew
(2021).
Influence of instability modes on cooling performance in hypersonic boundary layer with slot injection.
Aerospace Science and Technology, 109: 106409.
CERMINARA, Adriano, DEITERDING, Ralf and SANDHAM, Neil
(2020).
A mesoscopic modelling approach for direct numerical simulations of transition to turbulence in hypersonic flow with transpiration cooling.
International Journal of Heat and Fluid Flow, 86: 108732.
CERMINARA, Adriano and SANDHAM, Neil
(2020).
Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise.
Journal of Fluid Mechanics, 896: A21.