Active Physics & Astronomy Materials & Manufacturing

Multi-body Hypersonic Aerodynamics

In plain English

AI plain-English summary

When a missile or rocket stage separates at hypersonic speeds—above five times the speed of sound—the shockwaves from each body can slam into the other, potentially causing collision or structural failure. This project tackles a gap in fundamental understanding: how multiple objects interact aerodynamically when they separate at extreme speeds. Current design rules for multibody separation rely heavily on expensive flight tests or simplified models that miss complex shockwave interference. The researchers will use Cranfield’s hypersonic gun tunnel to physically measure these interactions with static models, and pair those experiments with high-order computer simulations that model both the fluid dynamics and the changing trajectories of separating bodies. The work is fundamental science. It does not aim to produce a new material or device. But a deeper, validated understanding of multibody hypersonic aerodynamics could improve the reliability of missile systems, re-entry vehicles, and future space launch stages. Similar fundamental research into shockwave interactions has previously enabled safer supersonic aircraft designs and more efficient rocket staging. Here, the payoff is safer, more predictable separation events in defence and aerospace applications—systems most people never see, but which depend on getting this physics exactly right.

View original technical description
The overall aim of the research is to investigate what are the aerodynamic interference characteristics, at hypersonic speeds, that are likely to adversely affect multibody separation. The research encompasses experimental and computational elements to evaluate the aerodynamics of multibody separation. Experiments using canonical configurations in the Cranfield hypersonic gun tunnel will statically represent the multi-body aerodynamics. The computational work will use Cranfield's high-order UCNS3D code to simulate hypersonic multi-body aerodynamic interactions and coupled trajectory modelling.

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Researchers

William PICARIELLO (Student)

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