School of Engineering and Information Technology


In-flight Mapping of Heating on a Hypersonic Vehicle

(Neely, Choudhury)

In collaboration with DSTO the HIFiRE-0 hypersonic test flight vehicle was instrumented with patches of permanent-change thermal paint and was launched from the Woomera test range in May 2009. This was the first in-flight test of the use of permanent-change thermal paints by UNSW@ADFA to map the extreme aerodynamic heating on hypersonic vehicles. The vehicle was recovered from the Woomera desert in August 2010 and the flight of the vehicle and the subsequent response of the paints was modelled using numerically based simulations of the fluid-thermal-structural interactions. This work was performed as part of a collaboration with A/Prof Riesen from PEMS, UNSW@ADFA and Dr. Paull and Dr. Odam from DSTO.



 Return to High Speed Flows and Microfluidics homepage
 Return to Research homepage

Other topics for High Speed Flows and Microfluidics during 2011:

 The world’s fastest spark plug
 Laser-Induced Plasmas at 100.000° Celsius
 Modelling of flow in a micro-hydrocyclone
 Sustainability in micro-manufacturing
 Multiphase flow mixing in a rotary holding furnace
 Projectiles in transonic and supersonic ground effect
 Time-resolved Mach-Zehnder interferometry
 Fluid-Structure Interaction of Gas Turbine Blades
 Base Flows
 Computational Studies of Hypersonic High Enthalpy Separated Flows
 Quantifying Exhaust Flows
 Laser-based Sensors for Safer Air Travel
 Free flying models in hypersonic facilities