In this paper, results from two experiments performed at California Institute of Technology’s T5 free-piston reflected shock tunnel are compared to numerical stability computations conducted using various stability analysis tools. The goal of this comparison is to begin understanding the range of boundary-layer transition predictability using different stability approaches for high-enthalpy flows. The analysis is focused on the physics of the second-mode instability at high enthalpy and the role of high-temperature effects. Although the stability solvers considering thermochemical nonequilibrium were best at estimating the measured second-mode frequency ( for shot 2990, for shot 3019), they overpredicted the most amplified frequency by approximately 16–23%. A moderate spread in the predicted most amplified frequency was also observed between the different solvers. The solvers estimated a most amplified frequency range of approximately 1450–1550 kHz for shot 2990 and approximately 1525–1650 kHz for shot 3019. There was also significant inconsistency observed in predicting the peak -factor magnitude, ranging from for shot 2990 and from for shot 3019.
High-Enthalpy Effects on Hypersonic Boundary-Layer Transition: Experimental and Numerical Comparison
AIAA Journal ; 1-11
01.04.2025
Aufsatz (Konferenz) , Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch