A nonlinear model, based on the area difference elasticity theory, has been developed to predict the sequence of stomatocyte–discocyte–echinocyte transformation in red blood cells. This model coarsely grains the cell membrane into a triangular network, accounting for the shear deformation of membrane skeleton, the area dilation, volume variation, bending deformation, and area difference deformation of lipid bilayer. It exhibits linear behavior under small deformations and transits to nonlinear behavior under large deformations, mirroring the biomechanical response of the cell that is susceptible to small deformations but significantly resists large deformations. The model parameters are calibrated by determining the biconcave equilibrium shape from an ellipsoidal stress-free configuration. After calibration, the model is utilized to predict the stomatocyte–discocyte–echinocyte transformation and is compared with the previously published experimental observations and the numerical results. It has been shown that the equilibrium shapes of a red blood cell are achieved in a self-equilibrium of spring lengths, as well as the balance between the triangle areas and surface area, and the interplay among dihedral curvature and area differences. The nonlinear model is believed to be capable of predicting the deformation behavior of red blood cells in diverse shape-transforming scenarios, such as in microvascular circulation and microfluidic devices.

Developing theoretical models to describe cell behavior is a crucial aspect in cell mechanics for gaining a deep understanding of the physical principles governing cellular processes. These models can provide a framework for predicting and analyzing cellular responses to various mechanical stimuli and environmental conditions, which is essential for various fields such as bioengineering, disease diagnostics and treatments, and drug development. Taking the deformation of red blood cells (RBCs), for example, a theoretical model can offer invaluable insights into the underlying mechanisms that enable RBCs to navigate through the complex vascular network and perform their pivotal role in oxygen transport. In addition, it can aid in predicting how changes in RBC mechanics may manifest in various diseases, such as anemia, sickle cell disease, and diabetes.

Currently, there are two main models for describing cell deformation, continuum, and discrete models.1–4 Continuum models treat the cell as a continuous material, applying principles of mechanics to understand how forces induce deformations.5–10 They often employ constitutive equations to describe the stress–strain relationships within the cell membrane, allowing for the analysis of large-scale deformations and overall cell behavior under various mechanical conditions. Among these equations, the neo-Hookean (NH) and Skalak (SK) laws are particularly prominent. The NK law assumes the membrane to be a three-dimensional isotropic and incompressible material, often used for vesicles,9 whereas the SK law assumes the membrane to be isotropic in its plane, initially proposed for RBCs.11 Discrete models, such as particle-based approaches, represent the cell membrane as a collection of interconnected particles or elements.12–17 Each particle follows specific physical laws, providing a detailed representation of the cell’s mechanical properties at a microscopic level. They often incorporate the microstructure of the membrane, offering deeper insights into the local deformations and structural changes within the cell. A cell membrane is comprised of three main components: the phospholipid bilayer, transmembrane proteins, and the skeleton.18,19 It is generally accepted that the lipid-bilayer contributes to the out-of-plane bending resistance and surface area incompressibility, while the skeletal spectrin network contributes to the in-plane shear deformation, and the cytoplasm contributes to the volume incompressibility of the cell.15 The discrete models allow to describe a more realistic and accurate RBC representation by incorporating the properties of these membrane components. While continuum models are favored for their computational efficiency and simplicity for large-scale analysis, discrete models provide a more detailed understanding of the micro-mechanical behavior of cells, making them widely used for studying specific cellular components or localized phenomena. Both continuum and discrete models have been extensively employed in analyzing cell deformation across various applications, such as blood-related diseases20–22 and cellular responses in microfluidic chips.23,24

In the present work, we aim to develop a nonlinear deformation model based on a discrete model, and investigate the red blood cell morphological transition. It is expected that the nonlinear model is more concise and more robust, offering a streamlined framework that not only accurately captures the essential characteristics of the cell deformation but also facilitates easier application in both research and practical scenarios.

In continuum models, a cell membrane is often assumed to be an infinitely thin sheet, and its motion is governed by the local equilibrium equation6,7,9
(1)
where s represents the gradient in the deformed configuration, τ is the Cauchy tension tensor, and q is the external load exerted by the surrounding fluids. Several constitutive laws have been used in the continuum models to formulate τ, which describe its principal components τ i ( i = 1,2) as a function of the principal stretch ratios λ i. Here, we list three widely used constitutive laws, where only τ 1 is given and τ 2 can be obtained by reversing the λ i subscripts.7 
  • The Hookean (HK) law
    (2)
    where G H K is the shear modulus and ν is the surface Poisson ratio.
  • The neo-Hookean (NH) law
    (3)
    where G N H is the associated shear modulus.
  • The Skalak (SK) law
    (4)
    where G S K is the associated shear modulus and C is a parameter to control the surface area dilation.

The HK law assumes that the membrane tensions depend linearly on the surface strain, while the NH law shows a nonlinear dependence but without an explicit parameter to control the area dilatation. The SK law not only provides a nonlinear dependence on shear deformation but also has an explicit parameter C to control the area dilation. Several studies have shown that both the NH and SK laws are close to the HK law in the small-deformation regime, while in the large-deformation regime, the NH law is strain-softening but the SK law is strain-hardening.7,25 Hence, the SK law may be more accurate to model the RBC deformation because available experiments suggest that the RBC membrane is strain hardening.

In discrete models, a set of particles are distributed on a membrane to represent its actin junctional complexes, and the connections between particles represent skeletal spectrin links. These connections form a two-dimensional triangle network, representing the cell membrane. Each particle follows Newton’s second law to obtain the RBC shape at equilibrium,10 
(5)
where t is the time, m and x i are the mass and position of the particle i, μ is the membrane viscosity, F i is the nodal force due to the cell deformation, and x i 0 and v i 0 are the initial conditions.
To describe the in-plane shear deformation, an in-plane shear energy is associated with spectrin links, and each link is treated as a linear or nonlinear spring. Here, we consider springs with a worm-like-chain attractive potential and a power repulsive potential13,26
(6)
where N s is the number of springs, k B T is the Boltzmann temperature, l max is the maximum allowable length for the springs, l j is the length of spring j, s j = l j / l max, p is the persistence length, k p is the power function coefficient, and q is the power index. When the attractive part is balanced with the repulsive part, an equilibrium length l 0 is achieved for each spring. A physical property, shear modulus k s, is associated with the in-plane shear energy in Eq. (6), given by13 
(7)
Similarly, to describe the out-of-plane bending resistance, an out-of-plane bending energy is associated with the spectrin links, primarily based on the Helfrich model.27 For a triangle network, the bending energy is given in discrete form as10,15,28,29
(8)
where k b is the bending coefficient, a j s is the local area occupied by the spring j, m j is the instantaneous curvature over the surface a j s, and m 0 is the corresponding spontaneous curvature. The curvature m j and area a j s are defined by
(9)
where θ j is the instantaneous angle between two neighboring triangles (labeled t 1 and t 2) sharing a common edge j, and a t 1 and a t 2 are the instantaneous area of the triangles t 1 and t 2, respectively.
The area and volume conservation constraints are often included in a discrete model to account for the incompressibility of the lipid bilayer and the inner cytosol, respectively. The area-constraint energy is defined by a penalty function13 
(10)
where k A and k a are the coefficients of total surface area and local triangle area, A and A 0 are the instantaneous and reference membrane surface areas, a j and a 0 are the instantaneous and reference areas of triangle j, and N t is the number of triangles. The volume-constraint energy is defined by13 
(11)
where k v is the coefficient of cell volume and V and V 0 are the instantaneous and reference volume of the cell.

Compared with the continuum model in Eq. (4), the discrete model in Eqs. (6)–(11) includes both the bending deformation and volume constraint, except the shear deformation and surface area constraint. The more constraints a deformation model integrates, the stronger its ability to distinguish cell shapes. Based on the theory of differential geometry, a surface is uniquely determined, up to isometry by its first and second fundamental forms. This means that if two surfaces have the same first and second fundamental forms, they are essentially identical. The shear energy U s is intended to constrain the arc (spring) length on the surface, and the area- and volume-constraint energies U a and U v are designed to restrain the surface area and volume, respectively. These geometric properties are associated with the first fundamental form of a surface. The bending energy U b is considered to constrain the surface curvature, which is related to the second fundamental form. Although Eqs. (6)–(11) are associated with the first and second fundamental forms of surfaces, they are still not sufficient to uniquely determine a surface. Hence, more constraints are required to be integrated into the continuum or discrete models.

Past studies30–36 have shown that the two leaflets of the membrane bilayer respond differently to various perturbations and remain coupled to each other. The expansion of the outer leaflet relative to the inner leaflet results in convex forms on the membrane surface and induces echinocytes. Similarly, the expansion of the inner leaflet relative to the outer leaflet results in concave forms on the membrane surface and induces stomatocytes. This is the well-known bilayer couple hypothesis, where area difference between two leaflets is the necessary and sufficient factor for shape changes. The area-difference-constraint energy is integrated by15,
(12)
where k a d and k a d are two area-difference-constraint coefficients, D 0 is the separation between two bilayer leaflets, Δ A and Δ A are the instantaneous area differences defined by
(13)
and Δ A 0 and Δ A 0 are the spontaneous area differences. Note that the two terms at the right-hand side of Eq. (12) are quite similar, and the difference lies in whether or not to take the absolute value. If only the first term is present, Δ A 0 can be achieved at multitude convex and concave combinations of triangular-pair arrangement over the membrane surface. To determine an unique combination, Geekiyanage et al.15 introduced one more term and called the total-membrane-curvature constraint, i.e., the second term in Eq. (12). We here combine this term into the area-difference constraint, instead of a separate constraint, because of the similarity between them. The first term at the right-hand side of Eq. (12) can be treated as a total direction-dependent curvature, while the second term can be regarded as a total direction-independent curvature. For convenience, the first term is here called direction-dependent area difference (DDAD), while the second term is called the direction-independent area difference (DIAD). At specified Δ A 0 and Δ A 0 , an unique convex and concave combination of triangular-pair arrangement can be obtained by integrating both the DDAD and DIAD constraints.15 
The total free energy of the membrane can, therefore, be determined by the summation of all the above energy components
(14)
and the force acting on the membrane particle i is given by37 
(15)
If more complex morphology of cells is desired, additional influencing factors should be identified and incorporated into existing models.
We develop a nonlinear deformation model on the basis of the discrete model. Note that the total free energy in Eq. (14) includes seven geometrical properties: the local properties of spring length l j, triangle area a j, and dihedral curvature m j and the global properties of surface area A, volume V, and area differences Δ A and Δ A . Therefore, our nonlinear model should include these properties at least. It is assumed that each geometric property exhibits the nonlinear force in the form
(16)
(17)
where k ^ φ and n ^ are model parameters, δ φ represents the variation of an arbitrary geometric property, δ φ L and δ φ U are the corresponding lower and upper limits. They are defined by
(18)
Notably, the force F ^ i becomes infinite as δ φ approaches either limit and is almost linear for small δ φ. It is important to acknowledge that our model does not account for all factors influencing cell morphology. For instance, internal cell structures such as the cytoskeleton and membrane dynamics can significantly affect the mechanical properties and, consequently, the cell equilibrium shape. Integrating these factors into one or more geometric properties presents a challenge, requiring further investigation into the relationship between cellular deformation mechanisms and geometric characterization.
Integrating Eq. (17) yields the corresponding free energy
(19)
where δ ψ is an integral variable. Moreover, by differentiating Eq. (17) and evaluating its value at φ = φ 0, we obtain the corresponding linear modulus
(20)
providing a way to determine k ^ φ and n ^ from the linear modulus K φ that is usually measured in experiments.
The limits δ φ L and δ φ U in Eq. (17) can be easily determined according to the physical constraints of each property. For example, a spring length is typically constrained with the limits of l L = α L l 0 and l U = α U l 0 with α L [ 0 , 0.8 ] and α U [ 2.2 , 3 ],13 such that δ l L = α L 1 and δ l U = α U 1. The area limits of a triangle can be expressed by the length limits
(21)
and thus δ a L = α L 2 1 and δ a U = α U 2 1. The limits of the total surface area are given by
(22)
with δ A L = α L 2 1 and δ A U = α U 2 1. The limits of the volume are given by the isoperimetric inequality
(23)
with δ V L = α L 3 1 and δ V U α U 3 1. The curvature limits are given by
(24)
such that δ m L = α U and δ m U = α U with a common assumption of m 0 = 0. The DDAD limits are set manually as
(25)
with δ Δ A L = ( β L 1 ) Δ A 0 / A 0 and δ Δ A U = ( β U 1 ) Δ A 0 / A 0 with the assumption of Δ A 0 0. Similarly, the DIAD limits are given by
(26)
with δ Δ A L = ( β L 1 ) Δ A 0 / A 0 and δ Δ A U = ( β U 1 ) Δ A 0 / A 0. These limits are summarized in Table I.
TABLE I.

The variation limits of geometrical properties, where αL and αU are the minimum and maximum variation ratio of a spring, and βL and βU are the minimum and maximum variation ratio of the area difference.

LimitδljδajδmjδAδVδΔAδΔA
Lower αL − 1  α L 2 1 αU  α L 2 1  α L 3 1 (βL − 1)ΔA0/A0 (βU − 1)ΔA0/A0 
Upper αU − 1  α U 2 1 αU  α U 2 1  α U 3 1 (βL − 1)ΔA0/A0 (βU − 1)ΔA0/A0 
LimitδljδajδmjδAδVδΔAδΔA
Lower αL − 1  α L 2 1 αU  α L 2 1  α L 3 1 (βL − 1)ΔA0/A0 (βU − 1)ΔA0/A0 
Upper αU − 1  α U 2 1 αU  α U 2 1  α U 3 1 (βL − 1)ΔA0/A0 (βU − 1)ΔA0/A0 
The parameters k ^ φ and n ^ can be directly determined by Eq. (20) using the given K φ. Nonetheless, for comparative purposes, we here derive these parameters by ensuring that our nonlinear model shares the same linear moduli as the discrete model in Eq. (14), i.e.,
(27)
Thus, the force strength coefficients are given by
(28)
For reference, their values for a healthy RBC are listed in Table II, where l 0 = 0.251 μm, a 0 = 0.0273 μm 2, A 0 = 140 μm 2, V 0 = 93.48 μm 3, and D 0 = 0.002 μm.
TABLE II.

The force strength coefficients in our nonlinear model for a healthy RBC with αL = 0.2, αU = 2.5, βL = 0.05, and βU = 15.

Discreteks (N/m)kb (J)ka (N/m)kA (N/m)kv (N/m)kad (J)kad (J)
Values2.5 × 10−632 2 × 10−1932 5 × 10−632 10−315 10215 7.5 × 10−1715 2.5 × 10−1715 
Nonlinear k ^ s (J) k ^ b (J) k ^ a (J) k ^ A (J) k ^ v (J) k ^ a d (J) k ^ a d (J)
n ^ = 1 1.9840 × 10−19 2.3578 × 10−17 1.1390 × 10−19 1.1682 × 10−13 8.7452 × 10−15 1.6172 × 10−13 0.5390 × 10−13 
n ^ = 2 1.0821 × 10−19 2.0326 × 10−17 0.9504 × 10−19 0.9747 × 10−13 8.1812 × 10−15 3.1713 × 10−18 1.0571 × 10−18 
n ^ = 3 0.5902 × 10−19 1.7522 × 10−17 0.7930 × 10−19 0.8134 × 10−13 7.6537 × 10−15 6.2191 × 10−23 2.0730 × 10−23 
Discreteks (N/m)kb (J)ka (N/m)kA (N/m)kv (N/m)kad (J)kad (J)
Values2.5 × 10−632 2 × 10−1932 5 × 10−632 10−315 10215 7.5 × 10−1715 2.5 × 10−1715 
Nonlinear k ^ s (J) k ^ b (J) k ^ a (J) k ^ A (J) k ^ v (J) k ^ a d (J) k ^ a d (J)
n ^ = 1 1.9840 × 10−19 2.3578 × 10−17 1.1390 × 10−19 1.1682 × 10−13 8.7452 × 10−15 1.6172 × 10−13 0.5390 × 10−13 
n ^ = 2 1.0821 × 10−19 2.0326 × 10−17 0.9504 × 10−19 0.9747 × 10−13 8.1812 × 10−15 3.1713 × 10−18 1.0571 × 10−18 
n ^ = 3 0.5902 × 10−19 1.7522 × 10−17 0.7930 × 10−19 0.8134 × 10−13 7.6537 × 10−15 6.2191 × 10−23 2.0730 × 10−23 

The nonlinear model in Eq. (16) is employed to reproduce the biconcave equilibrium shape of a RBC from an initial stress-free state (SFS). It is reported that the SFS shape is most likely to be an ellipsoid with a reduced volume ν in the range of 0.925–0.976 of a sphere having equivalent surface area,32 where the reduced volume is defined as ν = V 0 / ( 4 / 3 π R 0 3 ) and R 0 is an equivalent radius. We here choose v = 0.94,15 and the force strength coefficients are listed in Table II. The velocity-Verlet algorithm is used to numerically solve Eq. (5) with taking the initial conditions of x i 0 as the SFS shape and v i 0 = 0. In order to non-dimensionalize the simulation system, we choose the characteristic length, Boltzmann’s temperature, and mass as l = 1 μm, ε = 4.142 × 10 21 J, and m = 10 9 kg, respectively. The particle mass and viscosity are set as m = 10 9 kg and μ = 10 7 Pa s, and these values do not affect the equilibrium shape as they only dictate the convergence speed from the initial to the equilibrium state.10 

Figure 1 shows the shape evolution of a RBC from the initial SFS shape to a biconcave shape. The SFS shape is ellipsoidal, having A = 140 μm 2, V = 146 μm 3, and Δ A = Δ A = 0.17 μm 2, which is discretized into N v = 2562 membrane particles, N s = 7682 springs, and N t = 5120 triangles. Over time, the cell volume is gradually decreased with one side of the cell surface initially becoming concave. Subsequently, the opposite side of the cell surface also becomes concave, resulting in a biconcave shape with A = 140 μm 2, V = 93.48 μm 3, and Δ A = 0.172 μm 2 and Δ A = 0.254 μm 2. In our simulations, the global quantities, including A, V, Δ A, and Δ A , are progressively adjusted until they stabilize at their final values by t = 100. Hence, after t = 100, these global quantities are almost not changed any more, but the local quantities of l j, a j and m j are still varied. The simulation is ceased, and the equilibrium shape is acknowledged when the maximum global error
(29)
and the maximum local error
(30)
where the superscripts n and n + 1 denote two successive time steps, and the local quantities with bars represent the average values of their respective local variables.
FIG. 1.

(a) The shape evolution of a RBC from the initial ellipsoid to a biconcave shape, (b) the evolution of the surface area and volume, and (c) the evolution of the area differences, where A, Δ A, and Δ A are scaled by l 2, V is scaled by l 3, and t is scaled by l / ε / m .

FIG. 1.

(a) The shape evolution of a RBC from the initial ellipsoid to a biconcave shape, (b) the evolution of the surface area and volume, and (c) the evolution of the area differences, where A, Δ A, and Δ A are scaled by l 2, V is scaled by l 3, and t is scaled by l / ε / m .

Close modal

To calibrate the nonlinear model, we conduct comprehensive parametric studies, listed in Table III. Figure 2 shows the effect of shear modulus k s. Within the range k s [ 6.0 × 10 2 , 2.4 × 10 3 ], the RBC equilibrium shapes are nearly identical, exhibiting similar values of Δ A and Δ A . For k s 1.2 × 10 2, the biconcave shape becomes asymmetric, with one side less concave and the other side more concave. As k s exceeds 6.0 × 10 3 and increases further, the RBC shrinks with smaller radius. This is consistent with the fact that the spring becomes less extensible as the shear modulus is increased. Note that the linear shear modulus is measured in experiments about k s = 6.0 × 10 2 (i.e., 2.5 × 10 6 N/m) for a healthy RBC.32 

FIG. 2.

Effect of shear modulus k s, (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A, and (c) the comparisons of Δ A , where k s is scaled by ε / l 2.

FIG. 2.

Effect of shear modulus k s, (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A, and (c) the comparisons of Δ A , where k s is scaled by ε / l 2.

Close modal
TABLE III.

Parametric studies for model calibration, where the bold values represent the default setting.

Parameter Value 
k s ( ε / l 2 ) 1.2 × 102  6 × 10 2 1.2 × 103 2.4 × 103 6 × 103 1.2 × 104 2.4 × 104 6 × 104 
k b ( ε ) 4.8 9.6  4.8 × 10 1 9.6 × 101 3.84 × 102 1.92 × 103 3.84 × 103 9.6 × 103 
k a ( ε / l 2 ) 1.2 × 102 4.8 × 102 1.2 × 103 4.8 × 103 1.2 × 104  2.4 × 10 4 4.8 × 104 2.4 × 105 
k a d ( ε ) 1.8 × 101 9 × 101  1.8 × 10 2 1.8 × 103 9 × 103 1.8 × 104 9 × 104 1.8 × 105 
k a d ( ε ) 1.8 × 10−3 1.8 × 10−2 1.8 × 10−1 1.8 1.8 × 101  1.8 × 10 2 9 × 102 1.8 × 103 
αL  0.2 0.4 0.5 0.6 0.7 0.8 0.9 
αU 0.5 1.5  2.5 3.5 
βL  0.05 0.1 0.15 0.2 0.25 0.3 0.45 
βU 10  15 20 25 30 35 40 
Parameter Value 
k s ( ε / l 2 ) 1.2 × 102  6 × 10 2 1.2 × 103 2.4 × 103 6 × 103 1.2 × 104 2.4 × 104 6 × 104 
k b ( ε ) 4.8 9.6  4.8 × 10 1 9.6 × 101 3.84 × 102 1.92 × 103 3.84 × 103 9.6 × 103 
k a ( ε / l 2 ) 1.2 × 102 4.8 × 102 1.2 × 103 4.8 × 103 1.2 × 104  2.4 × 10 4 4.8 × 104 2.4 × 105 
k a d ( ε ) 1.8 × 101 9 × 101  1.8 × 10 2 1.8 × 103 9 × 103 1.8 × 104 9 × 104 1.8 × 105 
k a d ( ε ) 1.8 × 10−3 1.8 × 10−2 1.8 × 10−1 1.8 1.8 × 101  1.8 × 10 2 9 × 102 1.8 × 103 
αL  0.2 0.4 0.5 0.6 0.7 0.8 0.9 
αU 0.5 1.5  2.5 3.5 
βL  0.05 0.1 0.15 0.2 0.25 0.3 0.45 
βU 10  15 20 25 30 35 40 

Figure 3 shows the effect of bending modulus k b. Within the range k b [ 4.8 , 96 ], the RBC equilibrium shapes are nearly symmetrical and have the similar Δ A and Δ A . As k b exceeds 384 and continues to rise, the equilibrium shapes become less symmetric and more spherical. It is found that the bending modulus is a crucial factor in determining the local morphology of the equilibrium configuration. When it is large enough, the cell becomes so rigid that it rotates several rounds in the simulation domain. Consequently, the area differences Δ A and Δ A exhibit deviations from the reference values. Experimental measurements have determined the bending modulus to be k b = 48 ( 2.0 × 10 19 J).32 

FIG. 3.

Effect of bending modulus k b, (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A, and (c) the comparisons of Δ A , where k b is scaled by ε .

FIG. 3.

Effect of bending modulus k b, (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A, and (c) the comparisons of Δ A , where k b is scaled by ε .

Close modal
Figure 4 shows the effect of local area coefficient k a. It has almost no effect on the RBC equilibrium shape, with the similar area differences Δ A and Δ A , and a similar deformation index κ at the steady state. The deformation index is defined as38,39
(31)
where I 1, I 2, and I 3 are the principal moments of inertia of the cell, i.e., the eigenvalues of the moment-of-inertia tensor. It is equal to zero if a cell is spherical, and thus it is also called asphericity. The rounder a cell is, the smaller its asphericity. The slight difference is the mean triangle area, which results in a minor difference in the global surface area. Although k a has almost no effect on obtaining a biconcave equilibrium shape, it is usually set to be a very large value (e.g., k a = 2.4 × 10 415) for numerical stability in most of previous studies, especially for the cell experiencing significant deformation. However, Lim et al.32 suggested that a reasonable value for k a should be twice that of k s, otherwise the elasticity of membrane skeleton is overestimated.
FIG. 4.

Effect of local area modulus k a, (a) the comparisons of equilibrium shapes, (b) the comparisons of the mean local area a ¯, and (c) the comparisons of the deformation index κ, where k a is scaled by ε / l 2.

FIG. 4.

Effect of local area modulus k a, (a) the comparisons of equilibrium shapes, (b) the comparisons of the mean local area a ¯, and (c) the comparisons of the deformation index κ, where k a is scaled by ε / l 2.

Close modal

Figure 5 shows the effect of DDAD coefficient k a d. The RBC equilibrium shape is not significantly changed as k a d increases from 18 to 1.8 × 10 5. Previous studies31,32,40,41 have suggested that k a d should be of the same order as k b, so that the bending deformation results from the competition between membrane curvature and DDAD. However, Geekiyanage et al.15 have indicated that using k a d and k b on the same scale results in a significant difference between the reference DDAD and the instantaneous DDAD at equilibrium. Therefore, they recommended using a large value of k a d = 1.8 × 10 4 ( 7.5 × 10 17 J), which is considerably higher than k b. In such a condition, the bending energy can be considered negligible in comparison to the DDAD energy, which does not align with the effect of k b. Consequently, we recommend a middle value with k a d 3.75 k b in the present work.

FIG. 5.

Effect of DDAD coefficient k a d, (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A, and (c) the comparisons of κ, where k a d is scaled by ε .

FIG. 5.

Effect of DDAD coefficient k a d, (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A, and (c) the comparisons of κ, where k a d is scaled by ε .

Close modal

Figure 6 shows the effect of DIAD coefficient k a d . Within the range k a d [ 0.18 , 1800 ], the RBC equilibrium shapes are nearly identical, with the similar Δ A, Δ A , and κ. For k a d < 0.18, the equilibrium shape is no longer symmetrical, indicating that DIAD plays a non-negligible role in achieving the equilibrium shape. Moreover, Geekiyanage et al.15 have pointed out that the presence of DIAD can more accurately predict RBC shapes in agreement with experimental observations. We set k a d = k a d in the present work.

FIG. 6.

Effect of DIAD coefficient k a d , (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A , and (c) the comparisons of κ, where k a d is scaled by ε .

FIG. 6.

Effect of DIAD coefficient k a d , (a) the comparisons of equilibrium shapes, (b) the comparisons of Δ A , and (c) the comparisons of κ, where k a d is scaled by ε .

Close modal

Figure 7 illustrates the effects of the length limits α L and α U. Despite considerable adjustments to these limits, their effect is negligible, meaning that our nonlinear model is relatively insensitive to such variations for achieving a biconcave equilibrium shape. Likewise, the DDAD and DIAD limits β L and β U exert a negligible influence on the RBC equilibrium configuration, given that β L [ 0 , 0.45 ] and β U [ 5 , 40 ]. Moreover, the power n ^ does not significantly affect the biconcave equilibrium shape, if n ^ [ 1 , 4 ]. Hence, we set α L = 0.2, α U = 2.5, β L = 0.05, β U = 15, and n ^ = 2 as default values in the present work.

FIG. 7.

Effects of length limits (a) α L and (b) α U.

FIG. 7.

Effects of length limits (a) α L and (b) α U.

Close modal

Through the parametric analysis, it is demonstrated that the shear modulus k s affects the cell’s extensibility, and the bending modulus k b is pivotal in dictating local membrane bending. The local area coefficient k a, despite its minimal impact on the biconcave shape, is crucial for numerical stability, especially in cells undergoing significant deformation. The DDAD coefficient k a d and DIAD coefficient k a d are crucial for controlling the global concavity or convexity of the equilibrium shape. The parameters α L, α U, β L, and β U, which set the lower and upper bounds for geometric properties, exhibit a wide acceptable range, indicating the robustness of the nonlinear model.

It has been found that the normal biconcave shape of RBC can be modified into stomatocytes and echinocytes through a variety of agents, such as anionic amphipaths, high salt, high pH, and ATP depletion,15,36,42 known as stomatocyte–discocyte–echinocyte (SDE) transformation. Stomatocytes are cup-like concave shapes while echinocytes are crenated shapes with a spiculated cell surface. They are further categorized into subclasses I–IV, according to different levels of concavity and crenation.

We apply the nonlinear model to reproduce the SDE transformation, as shown in Fig. 8. The model’s predictions closely match the experimental observations and the numerical results of Geekiyanage et al.15 The slight differences with the experiments are caused by the parameter setting of Δ A and Δ A . Figure 9 shows quantitative comparisons of geometrical properties. During the transformation from the SFS ellipsoid to the discocyte, all the geometrical properties, except for V, undergo minor variations that are indicative of linear deformation. Consequently, the parameters determining the nonlinear behavior, such as δ φ L, δ φ U and n ^ in Eq. (17), exert only minor effects on the biconcave equilibrium shape. In contrast, the parameters directly associated with linear behavior, k ^ φ, have obvious effects on this shape. Likewise, for the equilibrium shapes of S I–III and E I, the geometrical properties of l ¯, a ¯, m ¯, A, Δ A, and Δ A also experience minor variations. As a result, the linear parameters k ^ φ have a pronounced effect, whereas the nonlinear parameters have a less noticeable impact. For the equilibrium shapes of S IV and E II–IV, the geometrical properties of m ¯, Δ A, and Δ A are largely varied, meaning that their deformation is in the range of nonlinear region. In such cases, the nonlinear parameters also have strong effects on their equilibrium shapes, especially for S IV and E IV. This is exactly the reason why most of previous model32,36 cannot predict the equilibrium shapes of S IV and E IV.

FIG. 8.

SDE transformation of RBC, (a) experimental observations,15 (b) simulation results from our nonlinear model, where the blue color indicates a negative curvature, and the red color indicates a positive curvature, (c) simulation results obtained by Geekiyanage et al.15 The symbol “S” at the top denotes stomatocyte, “D” denotes discocyte, and “E” denotes echinocyte.

FIG. 8.

SDE transformation of RBC, (a) experimental observations,15 (b) simulation results from our nonlinear model, where the blue color indicates a negative curvature, and the red color indicates a positive curvature, (c) simulation results obtained by Geekiyanage et al.15 The symbol “S” at the top denotes stomatocyte, “D” denotes discocyte, and “E” denotes echinocyte.

Close modal
FIG. 9.

Quantitative comparisons of geometrical properties, (a) average spring length l ¯, (b) average triangle area a ¯, (c) average dihedral curvature m ¯, (d) total membrane area A, (e) total cell volume V, (f) direction-dependent area difference Δ A, (g) direction-independent area difference Δ A , and (h) deformation index κ.

FIG. 9.

Quantitative comparisons of geometrical properties, (a) average spring length l ¯, (b) average triangle area a ¯, (c) average dihedral curvature m ¯, (d) total membrane area A, (e) total cell volume V, (f) direction-dependent area difference Δ A, (g) direction-independent area difference Δ A , and (h) deformation index κ.

Close modal

During the transformation from the discocyte to the stomatocyte, the value of Δ A gradually decreases, indicating an increasing concavity of the RBC. In contrast, Δ A is almost unchanged for S I–III, predominantly influencing the shape to have one concave side and one convex side. As the stomatocyte stage develops, the cup radius decreases, and several buds are formed inside the RBC. At the stage of S IV, the cell becomes more round, the cup is almost closed, and the interior buds are attached to the membrane. From the discocyte to the echinocyte, the value of Δ A gradually increases, indicating an increasing convexity of the RBC, as well as the Δ A . As the echinocyte stage develops, the spicules are formed over the membrane. At the stage of E IV, the cell also becomes round and a lot of sharp projections still attached on its surface. Therefore, both S IV and E IV have the nearly spherical shape, with the small deformation index κ, as shown in Fig. 9(h). All the equilibrium shapes have the same surface area A and volume V, yet they exhibit different curvature m ¯, which results in distinct area differences Δ A and Δ A .

It is known from the force magnitude in Eq. (17) that the nonlinear model exhibits linear behavior at δ φ 0 but demonstrates nonlinear behavior when δ φ approaches both the lower and upper limits δ φ L and δ φ U. This aligns with the biomechanical response of a cell susceptible to small deformation but significantly resists large deformation. For the linear deformation, such as S I, D, and E II, the force strength parameters k ^ φ have an obvious effect on the RBC equilibrium shape. In the case of nonlinear deformation, such as S IV and E IV, the nonlinear parameters, including lower limit δ φ L, upper limit δ φ U, and power index n ^, are also crucial in determining an equilibrium shape.

Considering the force direction in Eq. (16), the shear force of spring is directed along l j / x i. The forces resulting from local and global area variations are directed along a j / x i. The force due to volume variation is mainly directed along n j / x j, where n j is the outer normal to triangle j. Additionally, the forces arising from variations in dihedral curvature, DDAD and DIAD are directed along m j / x i. For an equilibrium configuration, the dihedral curvature, DDAD and DIAD are in a balanced state, meaning that bending deformation results from the competition among the local curvature, global DDAD, and global DIAD. Hence, assuming k a d k a d k b is not reasonable,15 as it overemphasizes the contribution of global DDAD and DIAD. It is widely recognized that the local curvature, global DDAD, and global DIAD are linked to the lipid bilayer, and consequently, the lipid bilayer is responsible for the bending deformation.15,32 The shear force is self-balancing among all the springs and does not directly compete with other forces. Since it is linked to the membrane skeleton, a SFS configuration characterized by a reference length l 0 is required to maintain its self-balance. Hence, the membrane skeleton is responsible for the shear deformation.

The forces arising from local and global area variations are in equilibrium, leading to the area dilation as a consequence of the competition between these areas. Lim et al.32 suggested that the local area is associated with the membrane skeleton, with k a 2 k s, contrasting with the majority of previous studies that recommended k a k A k s, implying a possible connection to the lipid bilayer. As shown in Fig. 4, the effect of k a on the discocyte’s equilibrium shape is negligible, given that the local area is almost unchanged. However, in situations where the local area experiences large fluctuations, such as in cases S IV and E IV, k a significantly influences the equilibrium shape, as shown in Fig. 10. At a small k a, the triangle area undergoes large fluctuations, and the force due to the local area variation is smaller than bending force. As a result, the interior buds and exterior spicules on the membrane is rounder at the small k a. It is observed that the results with k a k s are more consistent with experimental data than those with k a 2 k s. Therefore, we agree with the prevailing viewpoint that the local area is also linked to the lipid bilayer as the global area, such that the lipid layer contributes to the area dilation.

FIG. 10.

Effect of the force strength k a of local area, (a) the equilibrium shape of S IV, and (b) the equilibrium shape of E IV.

FIG. 10.

Effect of the force strength k a of local area, (a) the equilibrium shape of S IV, and (b) the equilibrium shape of E IV.

Close modal

The force due to volume variation does not compete with other forces. In fact, it is also different with other forces. Unlike the shear force, it is a global force and not requires the balance among all the local elements. Unlike the forces due to the global variations, such as global area, DDAD and DIAD, it does not compete with any other local forces, but an independent force, guiding the cell towards a reference volume V 0, either through contraction or expansion.

We have developed a nonlinear model to describe the cell deformation behavior, including the shear, bending, dilation, budding, and spiculation. The model exhibits linear behavior under small deformation but transits to nonlinearity under large deformations, precisely mirroring the biomechanical response of actual cells. Hence, the nonlinear model is accurate to capture stomatocyte–discocyte–echinocyte transformation with reasonable physical parameters. Additionally, the model incorporates seven geometrical parameters: spring length, triangle area, dihedral curvature, surface area, volume, direction-dependent area difference, and direction-independent area difference. These parameters are expressed in a unified mathematical framework, which endows the nonlinear model with conciseness and user-friendliness. Apart from those, we have observed that the model is insensitive to parameter variations when a cell experiences small deformation, exhibiting the low reliance on exact parameter specification.

In the present work, the nonlinear model has been applied to only reproduce the stomatocyte–discocyte–echinocyte transformation of RBCs. In near future, we anticipate expanding its application to additional scenarios, including cell deformation under shear flow, tube flow, and other relevant conditions. This extension will not only demonstrate the model’s versatility but also its potential to predict shape changes in other types of cells by recalibrating the geometrical parameters based on experimental data or theoretical considerations specific to the cell type of interest. We are confident that this model will facilitate a deeper understanding of cell mechanics and deformation responses.

The authors have no conflicts to disclose.

Sisi Tan: Conceptualization (lead); Data curation (lead); Formal analysis (lead); Funding acquisition (lead); Investigation (lead); Methodology (lead); Project administration (lead); Resources (lead); Software (lead); Supervision (lead); Validation (lead); Visualization (lead); Writing – original draft (lead); Writing – review & editing (lead).

The data that support the findings of this study are available within the article.

1.
C.
Lim
,
E.
Zhou
, and
S.
Quek
,
J. Biomech.
39
,
195
(
2006
).
2.
X.
Li
,
P. M.
Vlahovska
, and
G. E.
Karniadakis
,
Soft Matter
9
,
28
(
2013
).
3.
4.
M.
Ju
,
S. S.
Ye
,
B.
Namgung
,
S.
Cho
,
H. T.
Low
,
H. L.
Leo
, and
S.
Kim
,
Comput. Methods Biomech. Biomed. Eng.
18
,
130
(
2015
).
5.
D.
Barthès-Biesel
,
A.
Diaz
, and
E.
Dhenin
,
J. Fluid Mech.
460
,
211
(
2002
).
6.
E.
Lac
,
D.
Barthes-Biesel
,
N.
Pelekasis
, and
J.
Tsamopoulos
,
J Fluid Mech.
516
,
303
(
2004
).
7.
P.
Dimitrakopoulos
,
Phys. Rev. E
85
,
041917
(
2012
).
8.
X.-Q.
Hu
,
A.-V.
Salsac
, and
D.
Barthès-Biesel
,
J. Fluid Mech.
705
,
176
(
2012
).
9.
X.-Q.
Hu
,
B.
Sévénié
,
A.-V.
Salsac
,
E.
Leclerc
, and
D.
Barthès-Biesel
,
Phys. Rev. E
87
,
063008
(
2013
).
10.
K.-I.
Tsubota
,
J. Comput. Phys.
277
,
320
(
2014
).
11.
R.
Skalak
,
A.
Tozeren
,
R.
Zarda
, and
S.
Chien
,
Biophys. J.
13
,
245
(
1973
).
12.
I. V.
Pivkin
and
G. E.
Karniadakis
,
Phys. Rev. Lett.
101
,
118105
(
2008
).
13.
D. A.
Fedosov
,
B.
Caswell
, and
G. E.
Karniadakis
,
Comput. Method Appl. Mech. Eng.
199
,
1937
(
2010
).
14.
T.
Ye
,
N.
Phan-Thien
, and
C. T.
Lim
,
J. Biomech.
49
,
2255
(
2016
).
15.
N. M.
Geekiyanage
,
M. A.
Balanant
,
E.
Sauret
,
S.
Saha
,
R.
Flower
,
C. T.
Lim
, and
Y.
Gu
,
PLoS One
14
,
e0215447
(
2019
).
16.
T.
Ye
,
L.
Peng
, and
G.
Li
,
Biomech. Model. Mechanobiol.
18
,
1821
(
2019
).
17.
L.
Xiao
,
J.
Chu
,
C.
Lin
,
K.
Zhang
,
S.
Chen
, and
L.
Yang
,
Biomech. Model. Mechanobiol.
22
,
297
(
2023
).
19.
S.
Suetsugu
,
S.
Kurisu
, and
T.
Takenawa
,
Physiol. Rev.
94
,
1219
(
2014
).
20.
Y.
Imai
,
H.
Kondo
,
T.
Ishikawa
,
C. T.
Lim
, and
T.
Yamaguchi
,
J. Biomech.
43
,
1386
(
2010
).
21.
D. A.
Fedosov
,
W.
Pan
,
B.
Caswell
,
G.
Gompper
, and
G. E.
Karniadakis
,
Proc. Natl. Acad. Sci. U.S.A.
108
,
11772
(
2011
).
22.
T.
Ye
,
N.
Phan-Thien
,
B.
Cheong Khoo
, and
C.
Teck Lim
,
J. Appl. Phys.
115
,
224701
(
2014
).
23.
T.
Djukic
,
M.
Topalovic
, and
N.
Filipovic
,
J. Micromech. Microeng.
25
,
084012
(
2015
).
24.
P.
Balogh
and
P.
Bagchi
,
Biophys. J.
113
,
2815
(
2017
).
25.
M.
Pepona
,
J.
Gounley
, and
A.
Randles
,
Comput. Math. Appl.
132
,
145
(
2023
).
26.
T.
Ye
,
N.
Phan-Thien
,
C. T.
Lim
,
L.
Peng
, and
H.
Shi
,
Phys. Rev. E
95
,
063314
(
2017
).
27.
A.
Guckenberger
and
S.
Gekle
,
J. Phys.: Condens. Matter
29
,
203001
(
2017
).
28.
G.
Gompper
and
D.
Kroll
,
J. Phys. I
6
,
1305
(
1996
).
29.
30.
M. P.
Sheetz
and
S.
Singer
,
Proc. Natl. Acad. Sci. U.S.A.
71
,
4457
(
1974
).
31.
L.
Miao
,
U.
Seifert
,
M.
Wortis
, and
H.-G.
Döbereiner
,
Phys. Rev. E
49
,
5389
(
1994
).
32.
G. H. W.
Lim
,
M.
Wortis
, and
R.
Mukhopadhyay
,
Proc. Natl. Acad. Sci. U.S.A.
99
,
16766
(
2002
).
33.
R.
Mukhopadhyay
,
H. G.
Lim
, and
M.
Wortis
,
Biophys. J.
82
,
1756
(
2002
).
34.
K. D.
Tachev
,
K. D.
Danov
, and
P. A.
Kralchevsky
,
Colloids Surf., B
34
,
123
(
2004
).
35.
S. V.
Rudenko
,
Biochim. Biophys. Acta
1798
,
1767
(
2010
).
36.
M.
Chen
and
F. J.
Boyle
,
J. Biomech. Eng.
139
,
121009
(
2017
).
37.
G.
Závodszky
,
B.
Van Rooij
,
V.
Azizi
, and
A.
Hoekstra
,
Front. Physiol.
8
,
563
(
2017
).
38.
H.
Noguchi
and
G.
Gompper
,
J. Phys.: Condens. Matter
17
,
S3439
(
2005
).
39.
T.
Ye
,
X.
Zhang
,
G.
Li
, and
S.
Wang
,
Phys. Rev. E
102
,
042410
(
2020
).
40.
U.
Seifert
,
K.
Berndl
, and
R.
Lipowsky
,
Phys. Rev. A
44
,
1182
(
1991
).
41.
Z.-X.
Tong
,
X.
Chen
,
Y.-L.
He
, and
X.-B.
Liao
,
Phys. A
509
,
1183
(
2018
).
42.
W. H.
Reinhart
and
S.
Chien
,
Am. J. Hematol.
24
,
1
(
1987
).