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Luke Doherty

Dr

Luke Doherty PhD, BEng/BSc, AIAA Member

Departmental Lecturer in High Speed Flows

Biography

Dr Luke Doherty has been appointed as a Departmental Lecturer in High Speed Flows, continuing to lend his extensive experience in experimental hypersonic aerodynamics to the department. He graduated in 2008 from The University of Queensland, Australia with Bachelor of Engineering (Hons I) and Bachelor of Science degrees. He then completed his doctorate at the same university within the Centre for Hypersonics, measuring aerodynamic forces on an airframe integrated scramjet engine in the T4 Shock Tunnel Facility.

Joining the Oxford Thermofluids Institute in 2014 as a post-doctoral researcher, and then as a Senior Researcher in 2018, he has spent the last 8 years developing, commissioning and managing the Oxford High Speed Facilities – the T6 Stalker Tunnel, the High Density Tunnel and, more recently, the Low Density Tunnel; unique facilities which have placed Oxford at the forefront of high-speed experimental research.

Most Recent Publications

Experimental Simulation of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel

Experimental Simulation of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel

Heat transfer measurements of a transpiration-cooled stagnation point in transient hypersonic flow

Heat transfer measurements of a transpiration-cooled stagnation point in transient hypersonic flow

The UK National Wind Tunnel Facility

The UK National Wind Tunnel Facility

Laminar transpiration cooling experiments in hypersonic flow

Laminar transpiration cooling experiments in hypersonic flow

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation

View all

Research Interests

  • Short duration facility development (operation and diagnostics)
  • Aerodynamic force measurement techniques
  • Magnetic suspension and balance systems
  • Rarefied flows and satellite demise re-entry aerothermodynamics
  • High-speed inlet performance

Most Recent Publications

Experimental Simulation of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel

Experimental Simulation of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel

Heat transfer measurements of a transpiration-cooled stagnation point in transient hypersonic flow

Heat transfer measurements of a transpiration-cooled stagnation point in transient hypersonic flow

The UK National Wind Tunnel Facility

The UK National Wind Tunnel Facility

Laminar transpiration cooling experiments in hypersonic flow

Laminar transpiration cooling experiments in hypersonic flow

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation

View all

Most Recent Publications

Experimental Simulation of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel

Experimental Simulation of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel

Heat transfer measurements of a transpiration-cooled stagnation point in transient hypersonic flow

Heat transfer measurements of a transpiration-cooled stagnation point in transient hypersonic flow

The UK National Wind Tunnel Facility

The UK National Wind Tunnel Facility

Laminar transpiration cooling experiments in hypersonic flow

Laminar transpiration cooling experiments in hypersonic flow

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation

View all