One design factor that sets hypersonic vehicles apart from others is the consideration of aerothermal shape distortion. When flying at hypersonic speeds, the intense heat can cause a loss of structural rigidity, which, when combined with the pressure loads on the vehicle, can result in deformation of the structure. This deformation may be entirely elastic, causing the vehicle to return to its original shape after a flight. However, during operation, it is crucial to monitor this phenomenon because aerothermal distortion of a hypersonic vehicle can lead to numerous undesirable and potentially catastrophic effects.
To ensure the safety and feasibility of future reusable hypersonic aircraft, it is essential to develop sensing technologies capable of monitoring this phenomenon during flight.
This project will focus on exploring different technologies and techniques to sense hypersonic vehicle shape distortion.
How to Apply
Express your interest in this project by emailing Dr Graham Wild. Include a copy of your CV and your academic transcript(s).
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