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September 5, 2025Open Access

A Computational Journey of Hypersonic Phenomenon Travelling Towards the Aerospace Horizons and Beyond

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Analysis demonstrates aerodynamic characteristics of re-entry vehicles at various Mach numbers, highlighting scramjet applications.

Simulations reveal significant differences in drag between blunt and wedge-shaped re-entry vehicles, impacting performance.
The study evaluated aerodynamic characteristics using various turbulence models, focusing on simulations across multiple Mach numbers.
NASA Hyper X-43A scramjet models were adapted with injector modifications to assess thrust and stability of detonation waves.
Findings may influence future designs of hypersonic vehicles and techniques for enhancing thrust and specific impulse.

Pradyumna Rangnath Surwase (2025) studied this question.

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