Morphology and Mach Number Distribution of Merger Shock Surfaces in Merging Galaxy Clusters

Abstract In a binary merger of two subclusters with comparable masses, a pair of merger shocks are typically generated, often manifesting as double radio relics. Using cosmological hydrodynamic simulations, we identify major merger events with mass ratio <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:mn>1</mml:mn> <mml:mo>&lt;</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>1</mml:mn> </mml:mrow> </mml:msub> <mml:mo>/</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> </mml:msub> <mml:mo>≲</mml:mo> <mml:mn>4</mml:mn> </mml:math> and impact parameter b / r vir,1 ≲ 1, where r vir,1 is the virial radius of the heavier subcluster. We analyze merger shock surfaces approximately 1 Gyr after the pericenter passage, focusing on their morphology and the distribution of the Mach number, M s , of their constituent shock zones. The shock surfaces exhibit an elongated shape with a minor-to-major axis ratio of ∼0.6–0.9 and cover the area of ∼5%−20% of the enclosed sphere. The area ratio of the two shock surfaces roughly scales as <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mi>A</mml:mi> </mml:mrow> <mml:mrow> <mml:mi mathvariant="normal">ss</mml:mi> <mml:mo>,</mml:mo> <mml:mi mathvariant="normal">2</mml:mi> </mml:mrow> </mml:msub> <mml:mo>/</mml:mo> <mml:msub> <mml:mrow> <mml:mi>A</mml:mi> </mml:mrow> <mml:mrow> <mml:mi mathvariant="normal">ss</mml:mi> <mml:mo>,</mml:mo> <mml:mi mathvariant="normal">1</mml:mi> </mml:mrow> </mml:msub> <mml:mo>∝</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>1</mml:mn> </mml:mrow> </mml:msub> <mml:mo>/</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> </mml:msub> </mml:math> , typically positioning the larger shock ahead of the lighter subcluster. The axis connecting the two subclusters generally does not pass through the centers of the shock surfaces, due to the nonzero impact parameter and ambient turbulent flows. The distribution of M s of shock zones on each surface can be approximated by a log-normal function, peaking at M s ,peak ≈ 2−4.5 and extending up to ∼10. The surface-area-weighted and X-ray- emissivity-weighted average Mach numbers are comparable, with <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mi>M</mml:mi> <mml:mi>s</mml:mi> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mi>area</mml:mi> </mml:msub> <mml:mo>≈</mml:mo> <mml:mn>2.3</mml:mn> <mml:mo>–</mml:mo> <mml:mn>4.4</mml:mn> </mml:math> and <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mi>M</mml:mi> <mml:mi>s</mml:mi> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mi>X</mml:mi> </mml:msub> <mml:mo>≈</mml:mo> <mml:mn>2</mml:mn> <mml:mo>–</mml:mo> <mml:mn>4</mml:mn> </mml:math> . In contrast, the cosmic-ray energy flux-weighted average Mach numbers are higher with <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mi>M</mml:mi> <mml:mi>s</mml:mi> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mi>CR</mml:mi> </mml:msub> <mml:mo>≈</mml:mo> <mml:mn>3</mml:mn> <mml:mo>–</mml:mo> <mml:mn>5</mml:mn> </mml:math> . This discrepancy aligns with the differences between Mach numbers derived from X-ray and radio observations of radio relic shocks. On the other hand, we find that mostly <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mrow> <mml:mi>M</mml:mi> </mml:mrow> <mml:mrow> <mml:mi>s</mml:mi> </mml:mrow> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mrow> <mml:mi>X</mml:mi> </mml:mrow> </mml:msub> <mml:mo>≳</mml:mo> <mml:mn>2</mml:mn> </mml:math> for simulated merger shocks, although shocks with M X-ray ≲ 2 are often reported in observations.

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Publication Details

Journal
The Astrophysical Journal
Published
2024-12-31
DOI
https://doi.org/10.3847/1538-4357/ad98f7
Citations
4
Primary Topic
Galaxies: Formation, Evolution, Phenomena
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article
Field-Weighted Citation Impact
1.33

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article

Morphology and Mach Number Distribution of Merger Shock Surfaces in Merging Galaxy Clusters

Hyesung Kang, Eunyu Lee, Dongsu Ryu
4 citations
The Astrophysical Journal
Galaxies: Formation, Evolution, Phenomena
1.33
article

Morphology and Mach Number Distribution of Merger Shock Surfaces in Merging Galaxy Clusters

Hyesung Kang, Eunyu Lee, Dongsu Ryu
article en
4 citations

Abstract

Abstract In a binary merger of two subclusters with comparable masses, a pair of merger shocks are typically generated, often manifesting as double radio relics. Using cosmological hydrodynamic simulations, we identify major merger events with mass ratio <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:mn>1</mml:mn> <mml:mo>&lt;</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>1</mml:mn> </mml:mrow> </mml:msub> <mml:mo>/</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> </mml:msub> <mml:mo>≲</mml:mo> <mml:mn>4</mml:mn> </mml:math> and impact parameter b / r vir,1 ≲ 1, where r vir,1 is the virial radius of the heavier subcluster. We analyze merger shock surfaces approximately 1 Gyr after the pericenter passage, focusing on their morphology and the distribution of the Mach number, M s , of their constituent shock zones. The shock surfaces exhibit an elongated shape with a minor-to-major axis ratio of ∼0.6–0.9 and cover the area of ∼5%−20% of the enclosed sphere. The area ratio of the two shock surfaces roughly scales as <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mi>A</mml:mi> </mml:mrow> <mml:mrow> <mml:mi mathvariant="normal">ss</mml:mi> <mml:mo>,</mml:mo> <mml:mi mathvariant="normal">2</mml:mi> </mml:mrow> </mml:msub> <mml:mo>/</mml:mo> <mml:msub> <mml:mrow> <mml:mi>A</mml:mi> </mml:mrow> <mml:mrow> <mml:mi mathvariant="normal">ss</mml:mi> <mml:mo>,</mml:mo> <mml:mi mathvariant="normal">1</mml:mi> </mml:mrow> </mml:msub> <mml:mo>∝</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>1</mml:mn> </mml:mrow> </mml:msub> <mml:mo>/</mml:mo> <mml:msub> <mml:mrow> <mml:mi class="MJX-tex-calligraphic">M</mml:mi> </mml:mrow> <mml:mrow> <mml:mn>2</mml:mn> </mml:mrow> </mml:msub> </mml:math> , typically positioning the larger shock ahead of the lighter subcluster. The axis connecting the two subclusters generally does not pass through the centers of the shock surfaces, due to the nonzero impact parameter and ambient turbulent flows. The distribution of M s of shock zones on each surface can be approximated by a log-normal function, peaking at M s ,peak ≈ 2−4.5 and extending up to ∼10. The surface-area-weighted and X-ray- emissivity-weighted average Mach numbers are comparable, with <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mi>M</mml:mi> <mml:mi>s</mml:mi> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mi>area</mml:mi> </mml:msub> <mml:mo>≈</mml:mo> <mml:mn>2.3</mml:mn> <mml:mo>–</mml:mo> <mml:mn>4.4</mml:mn> </mml:math> and <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mi>M</mml:mi> <mml:mi>s</mml:mi> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mi>X</mml:mi> </mml:msub> <mml:mo>≈</mml:mo> <mml:mn>2</mml:mn> <mml:mo>–</mml:mo> <mml:mn>4</mml:mn> </mml:math> . In contrast, the cosmic-ray energy flux-weighted average Mach numbers are higher with <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mi>M</mml:mi> <mml:mi>s</mml:mi> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mi>CR</mml:mi> </mml:msub> <mml:mo>≈</mml:mo> <mml:mn>3</mml:mn> <mml:mo>–</mml:mo> <mml:mn>5</mml:mn> </mml:math> . This discrepancy aligns with the differences between Mach numbers derived from X-ray and radio observations of radio relic shocks. On the other hand, we find that mostly <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <mml:msub> <mml:mrow> <mml:mo stretchy="false">〈</mml:mo> <mml:msub> <mml:mrow> <mml:mi>M</mml:mi> </mml:mrow> <mml:mrow> <mml:mi>s</mml:mi> </mml:mrow> </mml:msub> <mml:mo stretchy="false">〉</mml:mo> </mml:mrow> <mml:mrow> <mml:mi>X</mml:mi> </mml:mrow> </mml:msub> <mml:mo>≳</mml:mo> <mml:mn>2</mml:mn> </mml:math> for simulated merger shocks, although shocks with M X-ray ≲ 2 are often reported in observations.

The Astrophysical JournalVol. 978(2)
National Research Foundation of Korea
Openalex Percentile: Top 18%
Galaxies: Formation, Evolution, Phenomena
1.33
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