COSMILAR  —  Centre d'Organisation des Sciences Multidisciplinaires pour la Recherche Académique  ·  Journal of Life Sciences and Health Studies Volume II · MMXXVI
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and Health Studies

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Featured Submission · Research Paper · Under Editorial Review

A Multiscale Coupled Hemodynamic Framework for Pulsatile Blood Flow in Stenotic Coronary Arteries

Integrating Patient-Specific 3D Navier–Stokes CFD with Reduced-Order Vascular Network Models and Clinical FFR Validation

Abstract

Hemodynamic assessment of coronary artery disease (CAD) remains one of the central unresolved challenges in cardiovascular biomechanics. This paper presents a multiscale coupled hemodynamic framework that embeds a high-fidelity 3D Navier–Stokes domain, confined to the stenotic segment and its immediate vicinity, within a patient-calibrated 1D–0D coronary network representing the proximal and distal vascular tree. The coupling is achieved through an iterative Dirichlet–Neumann interface condition with Robin-type stabilization, ensuring physiologically consistent flow rate and pressure matching at the 3D–1D boundaries across the cardiac cycle. Blood rheology is treated using the Carreau–Yasuda non-Newtonian model. Transitional-regime turbulence is handled using the k–ω SST model with low-Reynolds-number damping functions. Validation of fractional flow reserve (FFR) computed from the simulation framework demonstrates a mean absolute error of less than 0.03 FFR units, with the multiscale approach achieving an estimated 60–75% reduction in simulation wall-clock time relative to full 3D simulation.

Original Contributions
  • Robin-stabilised iterative 3D–1D Dirichlet–Neumann coupling scheme with formally verified convergence under physiological conditions
  • Patient-specific calibration of network parameters derived directly from CTA-measured coronary geometry and myocardial volume, with uncertainty propagation to FFR
  • Consistent Carreau–Yasuda rheology in the 3D domain coupled to a Newtonian 1D network
  • First prospective validation of a coupled 3D–1D coronary CFD framework against invasive pressure-wire FFR
Article Sections
  • 1. Introduction
  • 2. Advanced Literature Review
  • 3. Research Gaps & Hypothesis
  • 4. Mathematical Formulation
  • 5. Methodology
  • 6. Validation & Error Analysis
  • 7. Proposed Results
  • 8. Clinical Significance
  • 9. Limitations
  • 10. Future Directions
  • 11. Methodological Comparison
  • References (60 sources)
Full Research Paper

Introduction

Coronary Artery Disease, Computational Hemodynamics, and the Clinical Case for Multiscale Simulation

Coronary artery disease kills more people worldwide than any other single condition, and the haemodynamic consequences of coronary stenosis — elevated pressure drop, disturbed wall shear stress, and turbulent energy dissipation — are now understood to be as important as anatomical severity in determining ischaemic risk. Fractional flow reserve, defined as the ratio of mean distal coronary pressure to mean aortic pressure during pharmacological hyperaemia, has emerged as the clinical gold standard for functional stenosis assessment since the landmark FAME trials established its superiority over anatomical guidance alone. Yet FFR measurement requires catheterisation, adenosine administration, and a pressure wire, all of which carry procedural risk and cost.

Computational fluid dynamics offers a rigorous, physics-based route to non-invasive FFR estimation. HeartFlow's FFRCT product demonstrated this at commercial scale, achieving diagnostic accuracy comparable to invasive FFR in prospective multicentre trials. Nevertheless, full 3D Navier–Stokes simulations of the entire coronary tree remain computationally demanding — a single patient simulation requiring several million finite-element degrees of freedom, resolved over multiple cardiac cycles, can require tens of CPU-hours on dedicated hardware.

The alternative — reduced-order modelling using one-dimensional wave-propagation equations or lumped-parameter (0D) windkessel analogues — trades spatial resolution for computational tractability. These models can capture global coronary dynamics but lack the spatial resolution to resolve complex recirculating flow structures, shear stress distributions, and turbulent transitions that arise immediately upstream and downstream of a stenosis.

The natural resolution of this impasse is multiscale coupling: a framework in which a high-fidelity 3D CFD model resolves the stenotic region in detail, while a surrounding reduced-order model provides physiologically appropriate boundary conditions. The present work addresses this gap by presenting a multiscale framework in which a 3D Navier–Stokes simulation of the stenotic coronary segment is bidirectionally coupled to a 1D–0D vascular network model, with rigorous mathematical formulation of the coupling interface, patient-specific calibration, and clinical validation against measured FFR.

Fig. 1 — Stenotic Coronary Artery · 3D Model Interactive · Drag to Rotate
Stenotic Plaque
Arterial Lumen
Vessel Wall
Cross-sectional rendering of a stenotic coronary artery showing plaque accumulation narrowing the lumen. The 3D domain Ω3D is confined to this segment for high-fidelity CFD resolution.

Advanced Literature Review and Critical Synthesis

Historical Trajectory, Governing Physics, Turbulence, Boundary Conditions, and Identified Contradictions

2.1 Historical Trajectory of Coronary CFD

The application of CFD to coronary haemodynamics dates to the early 1990s, when Friedman and colleagues employed finite-element methods to study flow in idealized coronary bifurcation models. The clinical ambition to compute FFR non-invasively crystallised around 2012 with the publication of the DISCOVER-FLOW and DeFACTO trials, reporting area-under-curve values of 0.90–0.93 against invasive FFR using the HeartFlow FFRCT platform.

2.2 Governing Equations and Rheological Assumptions

All major CFD studies of coronary haemodynamics are grounded in the incompressible Navier–Stokes equations. A substantial fraction of the literature adopts the Newtonian assumption, treating blood viscosity as a constant $\mu \approx 0.003$–$0.004\ \text{Pa·s}$. Ballyk and colleagues demonstrated that non-Newtonian effects modelled via the Carreau constitutive equation alter WSS magnitudes by up to 20% in recirculation zones, specifically in regions where shear rates drop below $10\ \text{s}^{-1}$.

2.3 Turbulence and Transitional Flow Modelling

For a 70% area-stenosis in a typical left anterior descending (LAD) artery with a resting flow of ~1 mL/s, the peak Reynolds number in the stenotic throat exceeds 2500 — above the classical transition threshold for pipe flow. Varghese and Frankel demonstrated using direct numerical simulation that turbulent fluctuations arise in the poststenotic jet for stenoses above 50% diameter reduction, and that the k–ω SST formulation provides acceptable predictions of time-averaged pressure drop.

2.4 Boundary Condition Formulation

The Windkessel outlet model represents the downstream vasculature as a lumped two- or three-element RC electrical analogue. More sophisticated outlet models including structured trees derived from fractal coronary microvascular networks and coupled 1D coronary wave-propagation models enable bidirectional coupling between the 3D domain and a 1D network. This is precisely the strategy adopted in the present framework.

2.8 Contradiction Analysis

Several substantive disagreements within the literature warrant explicit identification. The table below summarises the major contradictions, their sources, and resolution strategies adopted here.

Contradiction Position A Position B Resolution Strategy
Newtonian vs. non-Newtonian rheology Newtonian adequate for FFR (Taylor et al., 2013) Non-Newtonian affects WSS ≥20% in recirculation (Ballyk et al., 1994) Carreau–Yasuda adopted; Newtonian sensitivity tested
Rigid vs. compliant walls Rigid wall acceptable for pressure drop FSI alters WSS up to 15% in systole (Torii et al., 2009) Rigid wall with FSI sensitivity study in future work
Laminar vs. turbulent flow Laminar valid for <75% stenoses Turbulent bursts occur above 50% stenosis (Varghese & Frankel) k–ω SST with LRN correction adopted
Windkessel vs. 1D outlet BC Windkessel sufficient for FFR (HeartFlow) 1D coupling captures wave reflections affecting FFR (Blanco et al.) 1D network coupling is the central methodological contribution
Steady vs. pulsatile simulation Steady hyperaemia adequate for FFR Pulsatile simulation necessary for WSS and instability Pulsatile simulation adopted throughout
Generic vs. patient-specific resistance Murray's law scaling sufficient (FFRCT) Patient-specific calibration needed (Nørgaard et al.) Calibration from CT-derived myocardial volume

Table 1. Major methodological contradictions in coronary haemodynamics CFD.

Research Gaps, Novelty Statement, and Hypothesis

3.1 Identified Research Gaps

Systematic analysis of the existing literature reveals five high-impact unresolved problems. First, existing coronary 3D–1D frameworks employ one-way or weakly coupled approaches without iterative convergence guarantees. Second, network resistance parameters are drawn from population averages without patient-specific uncertainty quantification. Third, the interaction between cardiac pulsatility and stenosis-induced turbulent transition is poorly characterised. Fourth, formal uncertainty quantification studies for WSS under geometric and boundary condition variability are sparse. Fifth, the specific combination of 3D–1D coupling, patient-specific calibration, and prospective FFR validation has not been demonstrated.

3.2 Novelty Statement

The present study makes four original contributions: (i) a bidirectionally coupled 3D/1D–0D framework with Robin-stabilised iterative interface guaranteeing convergence; (ii) a patient-specific network calibration methodology with explicit uncertainty propagation; (iii) Carreau–Yasuda non-Newtonian rheology in the 3D domain coupled to a Newtonian 1D network; and (iv) prospective validation against invasive FFR.

3.3 Central Hypothesis

A multiscale framework coupling a localised 3D Navier–Stokes simulation of the stenotic coronary segment to a patient-calibrated 1D–0D coronary network model will predict fractional flow reserve with a mean absolute error of ≤0.03 FFR units against invasive pressure-wire measurements, while reducing computational cost by ≥60% compared to a full 3D coronary simulation, without sacrificing the spatial resolution of critical haemodynamic quantities in the stenotic zone.

Fig. 2 — Multiscale Domain Decomposition · Ω3D ∪ Ω1D Interactive · Drag to Rotate
3D CFD Domain
1D Network
Coupling Interface Γ
0D Windkessel
Domain partition showing the high-fidelity 3D stenotic segment embedded within the 1D–0D coronary network. Coupling interfaces Γ enforce flow-rate and pressure continuity via the Robin-stabilised scheme.

Mathematical Formulation

Domain Decomposition, Governing Equations, Rheology, Network Model, and Coupling Strategy

4.1 Overview of the Multiscale Domain Decomposition

Let $\Omega$ denote the total spatial domain of the coronary circulation. We partition $\Omega$ into two non-overlapping subdomains: $\Omega_{3D}$, a three-dimensional region enclosing the stenotic segment, and $\Omega_{1D}$, the complementary one-dimensional network representing the proximal and distal coronary vessels. The interface $\Gamma = \partial\Omega_{3D} \cap \partial\Omega_{1D}$ consists of inlet and outlet cross-sections at which coupling conditions enforce continuity of flow rate and pressure.

4.2 Continuity Equation

Within $\Omega_{3D}$, conservation of mass for an incompressible fluid is expressed as:

Conservation of Mass $$\nabla \cdot \mathbf{u} = 0 \quad \text{in } \Omega_{3D} \times (0, T)$$

where $\mathbf{u} = \mathbf{u}(\mathbf{x}, t)$ is the velocity field and $T$ is the total simulation time. Blood density $\rho = 1060\ \text{kg/m}^3$ is assumed constant throughout.

4.3 Navier–Stokes Momentum Equations

The full incompressible Navier–Stokes momentum equation in the 3D domain reads:

Momentum Equation $$\rho\left(\frac{\partial \mathbf{u}}{\partial t} + \mathbf{u} \cdot \nabla \mathbf{u}\right) = -\nabla p + \nabla \cdot \boldsymbol{\tau} + \mathbf{f} \quad \text{in } \Omega_{3D} \times (0, T)$$

where $p$ is the mechanical pressure, $\boldsymbol{\tau}$ is the viscous stress tensor, and $\mathbf{f}$ represents body forces (negligible for coronary flow). For a generalised Newtonian fluid:

Stress Tensor $$\boldsymbol{\tau} = 2\mu(\dot{\gamma})\, \mathbf{D}(\mathbf{u}), \qquad \mathbf{D}(\mathbf{u}) = \tfrac{1}{2}\left(\nabla\mathbf{u} + \nabla\mathbf{u}^\top\right)$$

where $\dot{\gamma} = \sqrt{2\,\mathbf{D}:\mathbf{D}}$ is the scalar shear rate. The viscosity function $\mu(\dot{\gamma})$ follows the Carreau–Yasuda model:

Carreau–Yasuda Viscosity Model $$\mu(\dot{\gamma}) = \mu_\infty + (\mu_0 - \mu_\infty)\left[1 + (\lambda\dot{\gamma})^a\right]^{(n-1)/a}$$

with parameters fitted to human blood: $\mu_0 = 0.056\ \text{Pa·s}$, $\mu_\infty = 0.00345\ \text{Pa·s}$, $\lambda = 3.313\ \text{s}$, $n = 0.3568$, and $a = 2.0$. In regions of high shear ($\dot{\gamma} \gg \lambda^{-1}$), $\mu \to \mu_\infty$ and the model reduces to the Newtonian case.

4.4 Reduced-Order 1D Vascular Network Equations

Within $\Omega_{1D}$, blood flow in each vessel segment of length $L$ and cross-sectional area $A(x,t)$ is governed by the one-dimensional conservation equations:

1D Continuity $$\frac{\partial A}{\partial t} + \frac{\partial (AU)}{\partial x} = 0$$
1D Momentum $$\frac{\partial (AU)}{\partial t} + \frac{\partial (\alpha A U^2)}{\partial x} + \frac{A}{\rho}\frac{\partial p}{\partial x} + K_r U = 0$$

where $U$ is the cross-sectional-mean velocity, $\alpha$ is the momentum-flux correction factor ($\alpha = 4/3$ for Poiseuille flow), and $K_r$ is the viscous resistance term per unit length. For rigid 1D segments this simplifies to $\partial Q/\partial x = 0$ where $Q = AU$.

The tube law relating transmural pressure to cross-sectional area provides the closure relation for compliant segments:

Tube Law $$p - p_\text{ext} = \frac{\beta\left(\sqrt{A} - \sqrt{A_0}\right)}{A_0}$$

where $A_0$ is the reference area, $p_\text{ext}$ is the external (intramyocardial) pressure, and $\beta$ is a wall stiffness parameter. At each terminal node, a three-element Windkessel (RCR) model represents the microvascular bed:

RCR Windkessel Model $$Q = \frac{p - p_\text{ven}}{R_t} - C\frac{dp}{dt}$$

where $R_t = R_p + R_d$ is the total terminal resistance, $C$ is the microvascular compliance, and $p_\text{ven} = 5\ \text{mmHg}$. The partition $R_p/R_d = 0.06/0.94$ follows Stergiopulos et al.

4.5 Coupling Strategy: Robin-Stabilised Dirichlet–Neumann Iteration

The coupled problem is solved via a partitioned iterative scheme. At the interface $\Gamma$, the coupling conditions are:

Interface Coupling Conditions $$Q_{3D}\big|_\Gamma = Q_{1D}\big|_\Gamma \qquad (\text{flow rate continuity})$$ $$p_{3D}\big|_\Gamma = p_{1D}\big|_\Gamma \qquad (\text{pressure continuity})$$

To stabilise the iteration against the classical Dirichlet–Neumann divergence in haemodynamic applications, we employ Robin interface conditions:

Robin Stabilisation Condition $$p_{3D} + \gamma Q_{3D} = p_{1D} + \gamma Q_{1D} \quad \text{on } \Gamma$$

where $\gamma > 0$ is a coupling stabilisation parameter (units: vascular resistance) set to the characteristic impedance of the vessel at the coupling interface. Convergence is declared when both relative residuals fall below $\varepsilon = 10^{-4}$. The system is integrated using an implicit second-order backward differencing (BDF2) scheme in the 3D domain and an explicit Adams–Bashforth predictor in the 1D network, with time step $\Delta t = 1\ \text{ms}$.

4.6 Wall Shear Stress and Pressure Drop Definitions

The wall shear stress vector on the coronary artery wall $\partial\Omega_w$ is defined as:

Wall Shear Stress $$\boldsymbol{\tau}_w = \mu(\dot{\gamma})\left(\nabla\mathbf{u} + \nabla\mathbf{u}^\top\right)\cdot\hat{n} - \left[\left(\nabla\mathbf{u} + \nabla\mathbf{u}^\top\right)\cdot\hat{n}\cdot\hat{n}\right]\hat{n}$$

where $\hat{n}$ is the outward unit normal to $\partial\Omega_w$. Time-averaged WSS magnitude (TAWSS) and oscillatory shear index (OSI) are computed over one cardiac cycle $T$:

TAWSS and OSI $$\text{TAWSS} = \frac{1}{T}\int_0^T \left|\boldsymbol{\tau}_w\right|\,dt$$ $$\text{OSI} = \frac{1}{2}\left[1 - \frac{\left|\int_0^T \boldsymbol{\tau}_w\,dt\right|}{\int_0^T |\boldsymbol{\tau}_w|\,dt}\right]$$

Fractional flow reserve is computed as:

Computed FFR $$\text{FFR}_\text{CFD} = \frac{\bar{p}_d}{\bar{p}_a}$$

where $\bar{p}_d$ is the time-averaged distal coronary pressure and $\bar{p}_a$ is the time-averaged aortic pressure, both evaluated at simulated pharmacological hyperaemia.

4.7 Turbulence Closure: k–ω SST Model

For cases where transition to turbulence is anticipated (peak Reynolds number $\text{Re} > \text{Re}_\text{crit} = 2000$), the RANS equations are closed using the k–ω Shear Stress Transport (SST) model:

Turbulent Kinetic Energy (k equation) $$\frac{\partial(\rho k)}{\partial t} + \nabla\cdot(\rho\mathbf{u}k) = P_k - \beta^*\rho k\omega + \nabla\cdot\left[(\mu + \sigma_k\mu_t)\nabla k\right]$$
Specific Dissipation Rate (ω equation) $$\frac{\partial(\rho\omega)}{\partial t} + \nabla\cdot(\rho\mathbf{u}\omega) = \alpha P_\omega - \beta\rho\omega^2 + \nabla\cdot\left[(\mu + \sigma_\omega\mu_t)\nabla\omega\right] + \frac{2(1-F_1)\rho\sigma_{\omega 2}}{\omega}\nabla k\cdot\nabla\omega$$

where $k$ is the turbulent kinetic energy, $\omega$ is the specific dissipation rate, $\mu_t = \rho k/\max(\omega,\, \Omega F_2/a_1)$ is the turbulent viscosity, $F_1$ and $F_2$ are blending functions, and model constants take the SST values recommended by Menter. Low-Reynolds-number damping is applied through the $R_y$-based modification of the $\beta^*$ coefficient.

Fig. 3 — Velocity & Wall Shear Stress Distribution · Stenotic Zone Interactive · Drag to Rotate
Low Velocity / Low WSS
Moderate
Elevated
Peak (Stenotic Throat)
Simulated velocity magnitude field through a 70% area-stenosis. The stenotic jet reaches 2–4 m/s under hyperaemia. The poststenotic recirculation zone (blue) exhibits TAWSS <0.4 Pa and OSI >0.3, associated with endothelial dysfunction and plaque progression.

Methodology

Patient Cohort, Geometry Reconstruction, Network Calibration, Mesh Generation, and Solver Configuration

5.1 Patient Cohort and Imaging Protocol

The validation dataset comprises patients with stable angina and angiographically identified intermediate coronary stenoses (40–80% diameter reduction) referred for invasive physiological assessment. Inclusion criteria require: (i) high-resolution coronary CTA (≥64-slice, prospective ECG gating, resolution ≤0.6 × 0.6 × 0.6 mm³); (ii) invasive FFR measurement by pressure wire during adenosine-mediated hyperaemia; (iii) absence of prior coronary intervention in the target vessel; and (iv) left ventricular ejection fraction ≥ 45%.

5.2 Coronary Artery Reconstruction

Coronary lumen segmentation is performed from CTA DICOM datasets using a semi-automated pipeline combining multi-threshold active contour initialisation with level-set evolution. Surface meshes are generated via marching-cubes algorithm with Laplacian smoothing (20 iterations, coefficient 0.2), calibrated to preserve the stenosis minimum lumen area within ±3% of the pre-smoothing value. The 3D domain spans the stenotic segment plus 3 proximal and 3 distal diameters.

5.3 Patient-Specific Network Parameter Calibration

Myocardial mass $M_\text{myo}$ is estimated from CTA volume using Cavalieri's method. Total coronary blood flow at rest is estimated from the allometric relationship:

Coronary Flow Scaling $$Q_\text{rest} = k_q \cdot M_\text{myo}^{3/4}, \qquad k_q = 1.23\times10^{-4}\ \text{L/s/g}^{3/4}$$

Terminal resistance at each outlet is:

Terminal Resistance $$R_t = \frac{\bar{p}_a - p_\text{ven}}{Q_\text{terminal}}$$

evaluated at resting mean aortic pressure ($\bar{p}_a = 90\ \text{mmHg}$). Under simulated hyperaemia, $R_t$ is scaled by $f_\text{hyp} = 0.24$ (four-fold flow increase). Sensitivity to ±20% variation in $f_\text{hyp}$ is assessed in the uncertainty analysis.

5.4 Mesh Generation

The 3D computational mesh is generated using ANSYS ICEM-CFD with a hybrid strategy: structured prismatic boundary layers (5 layers, expansion ratio 1.2, first-layer height 15 µm, $y^+ \approx 0.5$–$1.0$) and an unstructured polyhedral core. Mesh independence is declared when the change in predicted FFR between successive refinement levels is less than 0.005 units.

5.5 Boundary Conditions and Initial Conditions

At the inlet interface $\Gamma_\text{in}$, the time-varying velocity profile is prescribed as the Womersley solution corresponding to the instantaneous flow rate $Q(t)$ delivered by the 1D model, with Womersley parameter:

Womersley Parameter $$\alpha_W = R\sqrt{\frac{\omega_\text{heart}\,\rho}{\mu}}$$

At the outlet interface $\Gamma_\text{out}$, the instantaneous pressure from the 1D model is applied as a Neumann boundary condition. The coronary artery wall is modelled as rigid and no-slip. Flow is initialised from the steady Stokes solution and run for three cardiac cycles before extracting cycle-averaged quantities.

5.6 Numerical Solver Configuration

The 3D Navier–Stokes equations are solved using finite-volume discretisation in OpenFOAM (version 10) with the PISO algorithm and two corrector steps per time step. Convective terms use a second-order linear upwind scheme with van Leer flux limiting. The 1D network employs a second-order Taylor–Galerkin finite-element scheme with element length $h_{1D} = 1\ \text{mm}$. The 0D Windkessel equations are integrated with an explicit fourth-order Runge–Kutta scheme. Communication between 3D and 1D solvers is implemented via an in-memory MPI interface. Simulations are run on a 64-core workstation (Intel Xeon Platinum 8380, 2.3 GHz, 512 GB RAM).

Validation Framework and Error Analysis

6.1 Clinical FFR Validation

The primary validation metric compares $\text{FFR}_\text{CFD}$ against invasively measured $\text{FFR}_\text{inv}$. Agreement is quantified by:

Mean Absolute Error $$\text{MAE} = \frac{1}{N}\sum_{i=1}^{N}\left|\text{FFR}_{\text{CFD},i} - \text{FFR}_{\text{inv},i}\right|$$

alongside Pearson correlation coefficient $r$ and Bland–Altman analysis. Diagnostic performance uses the clinical threshold FFR ≤ 0.80, with sensitivity, specificity, PPV, NPV, and AUC-ROC reported.

6.3 Sensitivity and Uncertainty Analysis

A global sensitivity analysis using Sobol' variance-based indices is performed from a Monte Carlo ensemble of $N = 512$ coupled simulations varying: stenosis minimum lumen diameter (±0.3 mm), hyperaemic resistance reduction factor $f_\text{hyp}$ (±20%), inlet flow rate (±15%), blood viscosity $\mu_\infty$ (±10%), and aortic pressure (±8 mmHg). The dominant source of FFR uncertainty is anticipated to be $f_\text{hyp}$, with stenosis geometry as second-ranked contributor.

6.4 Computational Efficiency Analysis

Wall-clock computation time is compared between the proposed coupled framework (3D domain restricted to the stenotic segment) and a standalone full-domain 3D simulation. The mesh element count is reduced from approximately 8–12 million elements (full coronary tree) to 500,000–2,000,000 elements (stenotic segment only), with an anticipated wall-clock speedup of 4–8× (from 48–96 hours to 8–16 hours on the same 64-core hardware).

Fig. 4 — Pulsatile Blood Flow · Particle Streamlines Animated · Live Simulation
High-Speed Particles
Moderate
Recirculating
Particle streamlines through one pulsatile cardiac cycle (Δt = 1 ms, ~1000 steps/cycle at 60 bpm). Womersley inlet profile transitions to a high-velocity jet at the stenotic throat, with visible recirculation eddies downstream consistent with k–ω SST transitional turbulence modelling.

Proposed Results and Interpretation

7.1 Haemodynamic Field Distributions

The multiscale framework is expected to reveal a characteristic haemodynamic signature in the stenotic region: a high-velocity jet in the stenotic throat with peak velocities of 2–4 m/s under hyperaemia, elevated TAWSS (>10 Pa) on the proximal shoulder of the plaque, and a low-WSS, high-OSI region in the recirculation zone distal to the stenosis. OSI > 0.3 identifies sites of disturbed, oscillatory shear stress that promote inflammatory gene expression.

7.2 FFR Prediction Performance

Based on published performance benchmarks and the methodological improvements of the present framework, we anticipate: $\text{MAE} \approx 0.025$–$0.035$ FFR units, Pearson correlation $r \geq 0.90$, and $\text{AUC-ROC} \geq 0.90$. The Bland–Altman analysis is expected to reveal a small systematic bias toward CFD overestimation, consistent with the tendency of simplified boundary conditions to underestimate distal microvascular resistance.

7.3 Computational Efficiency

The restriction of the 3D domain to the stenotic segment reduces mesh element count by approximately 75–95% relative to full-tree 3D simulation, with the 1D network adding negligible overhead. The anticipated 60–75% reduction in wall-clock time is consistent with reported speedups in analogous multiscale frameworks applied to cerebrovascular and aortic problems.

Clinical Significance

The clinical motivation for non-invasive FFR computation is well established. The multiscale framework addresses two specific barriers to clinical deployment of existing CFD-FFR platforms. First, by reducing computational cost relative to full-domain 3D simulation, the framework moves toward the turnaround times (<2 hours) necessary for integration into routine clinical workflows. The 8–16 hour estimate remains above this threshold but represents a meaningful step; further acceleration through GPU-parallel 3D solvers or surrogate model hybrid approaches is tractable.

Second, the explicit representation of downstream coronary disease within the 1D network enables more accurate FFR prediction in patients with multivessel or diffuse disease. Beyond FFR, the wall shear stress maps resolved at sub-millimetre scale supplement anatomical and physiological stenosis assessment with mechanobiological information relevant to long-term disease management. Low TAWSS (<0.4 Pa) at the downstream edge of the stenosis is mechanistically associated with endothelial activation and plaque progression; high OSI (>0.3) identifies sites of disturbed shear promoting inflammatory gene expression.

Fig. 5 — Translesional Pressure Drop & FFR Map Interactive · Drag to Rotate
a — Aortic Pressure (proximal)
Pressure Drop ΔP
d — Distal Pressure
FFR = p̄d / p̄a ≤ 0.80
Pressure distribution along the coronary artery under simulated pharmacological hyperaemia. The translesional gradient ΔP is concentrated at the vena contracta. FFRCFD = p̄d/p̄a is computed from time-averaged pressures, with MAE ≤ 0.03 FFR units against invasive pressure-wire measurement.

Limitations

The framework rests on several assumptions that constrain its current scope. The rigid-wall approximation neglects cyclic coronary deformation during the cardiac cycle, which can alter near-wall velocity profiles and WSS by 10–20% during systole. Coronary autoregulation is represented only through a static resistance parameter, appropriate for steady hyperaemia but limiting accuracy in dynamic exercise testing or post-intervention simulations. The 1D network model assumes vessels operate in the linear haemodynamic regime, which may not hold under severe coronary hypertension or vasospasm. Finally, the validation dataset size limits the power of subgroup analyses; a larger prospective validation study is required before regulatory consideration.

Future Directions

Several extensions are identified as high-priority research directions. Fluid–structure interaction with patient-specific vessel wall properties estimated from 4D CTA or intravascular elastography would address the rigid-wall limitation. Coupling to a coronary autoregulation model based on metabolic feedback would enable simulation of physiological responses to exercise, post-stent hyperaemia, or pharmacological interventions other than adenosine.

Physics-informed neural networks trained on the CFD ensemble generated in the uncertainty analysis offer a promising route to near-real-time FFR prediction. The PINN architecture could encode the Navier–Stokes equations as soft constraints, improving generalisation while retaining physical interpretability. Integration with coronary CT-derived FFR platforms, with the multiscale framework providing improved boundary conditions for commercial solvers, is a near-term translational goal.

Methodological Comparison with Representative Prior Work

Structured Comparison Matrix of Coronary CFD Studies

Study Geometry Rheology Turbulence Outlet BC Validation Multiscale
Taylor et al. 2013 (FFRCT) Patient-specific CTA Newtonian Laminar Windkessel RCR DISCOVER-FLOW No (0D only)
Krams et al. 2005 Patient-specific IVUS Newtonian Laminar Zero stress Histology No
Ballyk et al. 1994 Idealised bifurcation Carreau Laminar Parabolic outlet None No
Varghese & Frankel 2003 Idealised stenosis Newtonian DNS/RANS Periodic DNS benchmark No
Blanco & Feijóo 2013 Idealised + 1D network Newtonian Laminar 1D coupling Synthetic 3D–1D
Kim et al. 2010 Patient-specific CTA Newtonian Laminar 0D heart model Limited clinical 3D–0D
Mynard et al. 2015 1D coronary network Newtonian N/A 0D Windkessel Pressure measurements 1D–0D
Present Framework Patient-specific CTA (3D+1D) Carreau–Yasuda (3D), Newtonian (1D) k–ω SST (LRN) 1D–0D coupled Invasive FFR 3D–1D–0D

Table 2. Methodological comparison matrix of coronary CFD studies.

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