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This is a Experimental Study study.

Boundary layer velocimetry in a detonation-driven hypersonic shock tunnel using NO laser-induced fluorescence

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Experimental exploration establishes boundary layer velocity profiles in hypersonic flows, indicating NO-LIF offers reliable performance.

The experiment establishes boundary layer velocity profiles demonstrating successful NO-LIF application for hypersonic flows.
Optimal freestream velocity of 3470.7 m/s achieved with 4.97% measurement uncertainty highlights NO-LIF precision.
Simulation results correlate closely with measured velocity profiles, affirming NO-LIF robustness in hypersonic environments.
Comprehensive analysis improves signal-to-noise ratios, ensuring accuracy in displacement determination during testing.

Wu et al. (2025) studied this question.

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