Momentum decomposition of the pressure field

The generative mechanism of the pressure field is fundamental in turbulence research and flow control, especially when subject to turbulent separation at high Reynolds numbers. To this end, we propose a physics-based framework—momentum decomposition of the pressure field—which uses the momentum equations to decompose the spatial pressure gradient into quantifiable momentum budgets. Each momentum budget corresponds to a distinct physical mechanism, enabling a rigorous decomposition and quantitative evaluation of the inherent mechanisms governing pressure generation. Incorporating results of a direct numerical simulation of laminar cylinder flow, this method is first demonstrated, after which the three-dimensional large eddy simulation results of a complex turbulent bluff body wake at <a:math xmlns:a="http://www.w3.org/1998/Math/MathML"> <a:mrow> <a:msub> <a:mtext>Re</a:mtext> <a:mi>D</a:mi> </a:msub> <a:mo>=</a:mo> <a:mn>1.88</a:mn> <a:mo>×</a:mo> <a:msup> <a:mn>10</a:mn> <a:mn>5</a:mn> </a:msup> </a:mrow> </a:math> are analyzed with a comparison of flow control. In the near wake, the bulk of low pressure originates from the streamwise convection of the centripetal flow outside the wake, which manifests as a streamline curvature effect from the term <b:math xmlns:b="http://www.w3.org/1998/Math/MathML"> <b:mrow> <b:mover> <b:mi>u</b:mi> <b:mo>¯</b:mo> </b:mover> <b:mi>∂</b:mi> <b:mover> <b:mi>v</b:mi> <b:mo>¯</b:mo> </b:mover> <b:mo>/</b:mo> <b:mi>∂</b:mi> <b:mi>x</b:mi> </b:mrow> </b:math> , while the pressure variation inside the wake receives main contributions from Reynolds stresses. Under flow control, due to the streamline curvature modification near the base edge, the pulsed jet produces favorable pressure gradients from the mean flow term <c:math xmlns:c="http://www.w3.org/1998/Math/MathML"> <c:mrow> <c:mover> <c:mi>u</c:mi> <c:mo>¯</c:mo> </c:mover> <c:mi>∂</c:mi> <c:mover> <c:mi>v</c:mi> <c:mo>¯</c:mo> </c:mover> <c:mo>/</c:mo> <c:mi>∂</c:mi> <c:mi>x</c:mi> </c:mrow> </c:math> contributing to the bulk of base-pressure recovery. Overall, the proposed framework provides a fundamental flow diagnostic tool and a rigorous foundation for designing and analyzing flow control strategies, since pressure control can be rationally linked to the momentum budgets manipulation, generally applicable to flow regimes governed by the Navier-Stokes equations.

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Publication Details

Journal
Physical Review Fluids
Published
2026-04-01
DOI
https://doi.org/10.1103/bbyr-wqyv
Primary Topic
Fluid dynamics and aerodynamics studies
Type
article
Field-Weighted Citation Impact
0.00

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article

Momentum decomposition of the pressure field

Anonymous
Physical Review Fluids
Fluid dynamics and aerodynamics studies
article

Momentum decomposition of the pressure field

Anonymous
article en

Abstract

The generative mechanism of the pressure field is fundamental in turbulence research and flow control, especially when subject to turbulent separation at high Reynolds numbers. To this end, we propose a physics-based framework—momentum decomposition of the pressure field—which uses the momentum equations to decompose the spatial pressure gradient into quantifiable momentum budgets. Each momentum budget corresponds to a distinct physical mechanism, enabling a rigorous decomposition and quantitative evaluation of the inherent mechanisms governing pressure generation. Incorporating results of a direct numerical simulation of laminar cylinder flow, this method is first demonstrated, after which the three-dimensional large eddy simulation results of a complex turbulent bluff body wake at <a:math xmlns:a="http://www.w3.org/1998/Math/MathML"> <a:mrow> <a:msub> <a:mtext>Re</a:mtext> <a:mi>D</a:mi> </a:msub> <a:mo>=</a:mo> <a:mn>1.88</a:mn> <a:mo>×</a:mo> <a:msup> <a:mn>10</a:mn> <a:mn>5</a:mn> </a:msup> </a:mrow> </a:math> are analyzed with a comparison of flow control. In the near wake, the bulk of low pressure originates from the streamwise convection of the centripetal flow outside the wake, which manifests as a streamline curvature effect from the term <b:math xmlns:b="http://www.w3.org/1998/Math/MathML"> <b:mrow> <b:mover> <b:mi>u</b:mi> <b:mo>¯</b:mo> </b:mover> <b:mi>∂</b:mi> <b:mover> <b:mi>v</b:mi> <b:mo>¯</b:mo> </b:mover> <b:mo>/</b:mo> <b:mi>∂</b:mi> <b:mi>x</b:mi> </b:mrow> </b:math> , while the pressure variation inside the wake receives main contributions from Reynolds stresses. Under flow control, due to the streamline curvature modification near the base edge, the pulsed jet produces favorable pressure gradients from the mean flow term <c:math xmlns:c="http://www.w3.org/1998/Math/MathML"> <c:mrow> <c:mover> <c:mi>u</c:mi> <c:mo>¯</c:mo> </c:mover> <c:mi>∂</c:mi> <c:mover> <c:mi>v</c:mi> <c:mo>¯</c:mo> </c:mover> <c:mo>/</c:mo> <c:mi>∂</c:mi> <c:mi>x</c:mi> </c:mrow> </c:math> contributing to the bulk of base-pressure recovery. Overall, the proposed framework provides a fundamental flow diagnostic tool and a rigorous foundation for designing and analyzing flow control strategies, since pressure control can be rationally linked to the momentum budgets manipulation, generally applicable to flow regimes governed by the Navier-Stokes equations.

Physical Review FluidsVol. 11(4)
Tongji University (CN), University of Liverpool (GB), Imperial College London (GB), Chalmers University of Technology (SE)
National Natural Science Foundation of China, China Postdoctoral Science Foundation, National Key Research and Development Program of China, Fundamental Research Funds for the Central Universities
Openalex Percentile: Top 27%
Fluid dynamics and aerodynamics studies
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