Receptivity and instability of the hypersonic flow over moderately blunt cones
N. d'Epr\'emesnil, C. Caillaud, G. Lehnasch, M. Olazabal, P. Jordan

TL;DR
This study uses resolvent analysis to investigate the receptivity and instability mechanisms in hypersonic flow over a blunt cone, revealing how wall temperature and entropy-layer effects influence mode amplification and transition processes.
Contribution
It provides new insights into the linear receptivity and amplification mechanisms in hypersonic blunt cone flows, highlighting the role of entropy-layer effects and wall temperature conditions.
Findings
Stationary streak modes are most amplified in isothermal conditions.
The first Mack mode dominates in adiabatic conditions.
Entropy-layer disturbances significantly influence receptivity structures.
Abstract
With a view to identifying and understanding the linear receptivity and amplification mechanisms that underpin laminar-to-turbulent transition over blunt bodies in hypersonic flow, we use resolvent analysis to study the flow over a blunt cone with 7{\deg} half-angle at Mach number , zero angle of attack, and nose-radius-based Reynolds number . Optimal forcing and responses are obtained for frequencies up to 330 kHz and azimuthal wavenumbers between 0 and 200. Wall-temperature effects are accounted for by considering both isothermal ( 300 K) and adiabatic wall conditions. The resolvent analysis shows that stationary streak modes are the most amplified in the isothermal case, followed by entropy-layer modes between 20 and 140 kHz. In the adiabatic case, the Mack mode is the most amplified. The entropy layer, caused by the nose-tip…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Computational Fluid Dynamics and Aerodynamics · Aerodynamics and Acoustics in Jet Flows
