Search arXiv⌕ Search

arXiv · 2610.20372

Component-wise outer similarity of turbulent boundary layers with strong adverse-pressure gradient

Abstract

The adverse-pressure-gradient (APG) effect challenges the classical scaling of turbulent boundary layers (TBLs) over a flat plate, and it remains unclear whether outer-layer similarity holds across a wide range of APG strengths.We assemble a benchmark comprising the present direct numerical simulation of a suction--blowing-induced separation bubble and published profiles, spanning Clauser parameters $β_e=0.04$--$180$ and Reynolds numbers $Re_θ=530$--$19000$. Across this broad $(β_e,Re_θ)$ parameter range, existing APG normalizations do not simultaneously collapse the two mean-velocity defects and four Reynolds-stress components, leaving open whether outer similarity persists. Instead of defining new scalings, we normalize each quantity by its value at a common location $y_s$. Results are shown using $y_s=0.5δ$, beyond the outer stress peaks. For each of the six quantities, the normalized profiles exhibit a common outer shape across the conditions, with collapse emerging for $y/δ\gtrsim0.2$ for the velocity defects and $y/δ\gtrsim0.4$ for the Reynolds stresses. The collapse-error analysis shows that outer self-similarity is retained over a broad range of $y_s$ within the outer region and is not restricted to $y_s=0.5δ$. Furthermore, explicit expressions are provided for the normalized outer profiles. These results support component-wise outer similarity under strong APGs and provide compact references for APG turbulence-model assessment and conditional profile reconstruction.

Explore related subjects

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Yu-Xuan Shi, Mingze Ma, Xi Chen. 2026-10-14. Component-wise outer similarity of turbulent boundary layers with strong adverse-pressure gradient. https://arxiv.org/abs/2610.20372

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related papers

Linear causality and stability constraints on relativistic second-order magnetohydrodynamics

In this work, we construct a theoretical framework for relativistic second-order magnetohydrodynamics based on entropy current analysis. The formalism consistently incorporates finite relaxation dynamics of the dissipative fluxes, providing a transient framework suitable for analyzing linear stability and short-wavelength causality. Utilizing linear mode analysis, we investigate the constraints imposed by causality and stability on this anisotropic system. By linearizing the theory around a homogeneous equilibrium state, we identify the magnetosonic, Alfvén, and charge-diffusion sectors, together with their coupling terms. For each sector, we derive asymptotic dispersion relations in both the long-wavelength (small-$k$) and short-wavelength (large-$k$) regimes, validating them against exact numerical roots. Our numerical analysis confirms the accuracy of these asymptotic solutions and uncovers a nontrivial angular dependence, especially near special propagation directions where the ordinary momentum expansion becomes less reliable. By evaluating the large-$k$ behavior of the propagating branches alongside the damping properties of non-hydrodynamic modes, we delineate the corresponding causality constraints. We find that the admissible linear causal domain is governed by the interplay between propagation direction, anisotropic transport coefficients, and relaxation times, with the resulting bounds being intrinsically mode-dependent. These findings provide a systematic theoretical basis for investigating linear stability and short-wavelength causality in relativistic magnetohydrodynamics beyond the first-order approximation.

physics.flu-dyn↗

An Omni-Temporal Framework for Hydrodynamic Dispersion and Reaction in Porous Media

Many applications involve porous-media transport driven on time scales comparable to the pore-scale diffusion time, for which classical pseudo-steady dispersion models based on time-invariant transport coefficients may become inaccurate. While frequency-dependent dispersion has been studied in non-reactive porous media, a corresponding framework that simultaneously accounts for advection, diffusion, and heterogeneous interfacial reaction remains lacking. We address this gap by introducing an omni-temporal framework based on volume averaging of the frequency-domain pore-scale advection-diffusion equation subject to a Robin boundary condition spanning the full range of interfacial reactivity. The resulting upscaled formulation yields four frequency-dependent transfer functions: a dispersion tensor, an advection-suppression vector, a spectral Sherwood number, and a reactivity-bias vector, with the reactivity-bias vector introduced here for the first time. Analytical solutions for fully developed flow between parallel plates and through circular tubes reveal distinct kinetics- and diffusion-limited regimes, including capacitive and semi-infinite Warburg-type frequency responses. Comparisons of transient breakthrough curves with direct numerical simulations demonstrate substantial improvement over conventional pseudo-steady dispersion, particularly for short-duration pulses. Application to a periodic array of square rods under cross flow further demonstrates the frameworks applicability beyond canonical geometries.

physics.flu-dyn↗

Comparative Numerical Study of Film Cooling Strategies for Thermal Protection of a Kerosene-Fueled Oblique Detonation Combustor

Thermal protection remains a major challenge for oblique detonation engines (ODEs), whose combustors combine intense heat release, anchored on oblique detonation waves (ODWs). This study numerically investigates the effects of coolant type and mass flow rate on the flow structure, thermal environment and propulsion performance of a film-cooled kerosene-air ODE combustor at Mach 10 and 15 km altitude. Three active cooling strategies are compared under identical conditions: air film cooling, gaseous-kerosene film cooling, and liquid-kerosene mist cooling. Stable, wall-attached oblique-detonation propagation and the canonical wave structure are maintained, with the wave-coolant interaction depending systematically on the coolant medium. Air injection causes the greatest disturbance to the initiation region and downstream wave interactions, yielding the largest propulsion penalty. The cooling strategies substantially reduce the near-wall thermal load but produce distinct wall-temperature distributions. Gaseous-kerosene cooling yields a spatially periodic response from the discrete injection slots, whereas liquid-kerosene mist cooling gives a smoother and lower near-wall temperature through two-phase mixing and phase-change heat absorption. Liquid-kerosene mist cooling provides the most favorable balance between thermal protection and propulsion performance at low to moderate injection levels. With further increases in injection level, the thermal benefit approaches saturation while the propulsion penalty continues to grow: the mean near-wall fluid temperature reduction remains about 87% across both the inter-slot and cooling-slot wall segments, whereas the total specific impulse is reduced by about 3%-5%. These results quantify the thermal-propulsive trade-off across film-cooling media and demonstrate the potential of fuel-based cooling for thermal management in hypersonic ODE combustors.

physics.flu-dyn↗