The terahertz detection performance and operating regimes of graphene plasmonic field-effect transistors (FETs) were investigated by a hydrodynamic model. Continuous wave detection simulations showed that the graphene response sensitivity is similar to that of other materials including Si, InGaAs, GaN, and diamond-based FETs. However, the pulse detection results indicated a very short response time, which favors rapid/high-sensitively detection. The analysis on the mobility dependence of the response time revealed the same detection regimes as the traditional semiconductor materials, i.e., the non-resonant (collision dominated) regime, the resonant ballistic regime, and the viscous regime. When the kinematic viscosity (ν) is above a certain critical viscosity value, νNR, the plasmonic FETs always operates in the viscous non-resonant regime, regardless of channel length (L). In this regime, the response time rises monotonically with the increase of L. When ν < νNR, the plasmonic resonance can be reached in a certain range of L (i.e., the resonant window). Within this window, the carrier transport is ballistic. For a sufficiently short channel, the graphene devices would always operate in the non-resonant regime, regardless of the field-effect mobility, corresponding to another viscous regime. The above work mapped the operating regimes of graphene plasmonic FETs and demonstrated the significance of the viscous effects for the graphene plasmonic detection. These results could be used for the extraction of the temperature dependences of viscosity in graphene.

Ever since the discovery, graphene has been the subject of great attention due to its unique electrical,1,2 mechanical,3,4 chemical,5 and thermal6 properties. One peculiar feature of graphene is that the electron–phonon scattering in graphene is weak, while the electron–electron collision is very frequent due to a small effective mass.7–10 This promotes hydrodynamic behavior and enables resonant plasmonic excitations in graphene samples.11 

Graphene-based plasmonic devices are promising for THz detection and optoelectronic applications as they offer long-lived, high-velocity plasmons and are highly tunable by gating and doping.11–15 Other merits of graphene device include the significant THz absorption,16 the ability of forming multi-layer structures,17 and the high sensitivity to chemicals and vapors.5,18 In those devices, the realization of plasmonic resonance is a key issue. Experimental studies showed that both the broadband (non-resonant)19,20 and resonant operation21were achievable in graphene plasmonic field-effect transistors (FETs), and these two detection modes are interconvertible via operating parameters.

Another important issue regarding graphene plasmonics is the viscosity effect. Due to strong electron–electron scattering, the shear viscosity in graphene is on the order of ∼0.01–0.1 m2/s, which is larger than the viscosity of honey.9,22,23 The electron flow in graphene could, therefore, behave like a classical viscous liquid and even lead to the formation of whirlpools.8,9,24 Consequently, the detection performance of graphene plasmonic devices will be affected. Our previous theory and measurements25 showed that high viscosity leads to the attenuation of the DC voltage response, thus limiting the sensitivity of the plasmonic THz detector. This is caused by an additional attenuation mechanism provided by the viscosity, which becomes non-negligible when the characteristic time L2/ν is close to or smaller than the momentum relaxation time, where L is the channel length and ν is the kinematic viscosity.25 The viscosity effect also broadens the plasmonic resonant peaks by Δωn ≈ νqn2, where qn = πn/L is the nth order wave number.26 Under the pulse detection mode, high viscosity results in a rapid decay of plasma waves and causes the saturation of the response time.27–30 

The aforementioned works revealed several important features of viscous plasmonic detection and laid the foundation for the viscous detection regime. However, those studies mostly focused on other material systems such as InGaAs and Si, while the viscosity effect in graphene plasmonic FETs was rarely studied or ignored.21 Moreover, the criteria and mechanisms of operating mode transitions in graphene plasmonic devices have not been established. Therefore, in this work, we focus on the detection of THz continuous wave (CW) and ultrashort pulse by monolayer graphene (MLG) and bilayer graphene (BLG) plasmonic FETs. The detection performance in both CW and pulsed conditions is simulated and analyzed. We also evaluate the dynamic boundaries for different detection regimes (collision dominated, ballistic, and viscous) and discuss the effect of viscosity on the mode conversion and response time alteration. Those efforts help map the operating regimes of graphene plasmonic FETs and specify the criteria of the regime conversion. We also discuss the possibility of the viscosity parameter extraction using the obtained results.

For a sufficiently long plasma channel, MLG and BLG follow a linear dispersion law,31–33ωp = sk, where ωp and s ≈ (e|U0|/m*)0.5 are the plasma frequency and velocity, respectively, and k is the wave vector. The carrier confinement and density of states are different in MLG and BLG. For MLG, the “fictitious” effective mass m* is a function of 2D carrier density (ns) given by m* = (ћ/VF)⋅(πns)0.5, where VF is the Fermi velocity on the order of ∼106 m/s.8,31,34 As a result, ωp ∼ U01/4. For BLG, the carrier effective mass is a much weaker function of ns and one can assume m* ≈ 0.036m0, where m0 is the mass of free electron, thus ωp ∼ U01/2.21,33 This shows that a BLG device has a better tunability by gate than a MLG device.

Now, we set up the mobility (μ) and viscosity (ν) model for MLG and BLG systems. According to previous reports,35–39 the mobility in graphene varies with carrier density ns, and the ns dependence law is drastically different in MLG and BLG. μ decreases quasi-exponentially with rising ns (or U0) in MLG,37–39 but it rises with an increase of ns in BLG.36 Besides, while the general variation tendencies are similar, the value of μ in different graphene samples could vary significantly, ranging from ∼0.01 m2/V s to ∼20 m2/V s.7,35,37,39–42 However, the ultra-high mobility level was most realized under some strict conditions, e.g., cryogenic temperature (below 4 K), almost-intrinsic sample (near charge neutrality point), ultra-clean condition, encapsulation, and complex deposition and epitaxy procedures.37,41,42 In this work, we follow the general ns dependence law proposed previously and adjust the amplitude of μ into a typical range (0.1–0.5 m2/V s).12,18,33,36,38,40 Such mobility setting may be arbitrary, but it helps us get a general variation trend and the typical order of responsivity in graphene FETs. The mobility models used are given in Fig. 1(a). As seen, when ns < 1012 cm−2, the MLG mobility is higher than that of BLG, and at higher ns, the mobility of BLG exceeds MLG.

FIG. 1.

The carrier density dependent models of (a) mobility and (b) viscosity used in our simulation at T = 300 K. In (a), the experimental data (scatters) are taken from Ref. 36and multiplied with certain factors (0.6 for MLG and 5 for BLG) to fit in the common mobility range (0.1–0.5 m2/V s). The solid curves are fittings. In (b), the experimental viscosity data for BLG (blue scatters) are taken from Ref. 9 and converted from 240 K to 300 K, assuming 1/[T2 ln(T/TF)] law.23,43 The solid curve is the fitting. In the simulation, we use fitting curves to calculate mobility and viscosity. The fitting equations are μMLG = 0.147 + 0.488 exp(−ns/0.721 × 1012) (m2/V s), μBLG = 0.0298 + 2.222 × 10−17ns − 2.99 × 10−34ns2 + 1.703 × 10−51ns3, νBLG = −0.0637 + 1.624 × 10−17ns − 6.582 × 10−34ns2 + 1.316 × 10−50ns3.

FIG. 1.

The carrier density dependent models of (a) mobility and (b) viscosity used in our simulation at T = 300 K. In (a), the experimental data (scatters) are taken from Ref. 36and multiplied with certain factors (0.6 for MLG and 5 for BLG) to fit in the common mobility range (0.1–0.5 m2/V s). The solid curves are fittings. In (b), the experimental viscosity data for BLG (blue scatters) are taken from Ref. 9 and converted from 240 K to 300 K, assuming 1/[T2 ln(T/TF)] law.23,43 The solid curve is the fitting. In the simulation, we use fitting curves to calculate mobility and viscosity. The fitting equations are μMLG = 0.147 + 0.488 exp(−ns/0.721 × 1012) (m2/V s), μBLG = 0.0298 + 2.222 × 10−17ns − 2.99 × 10−34ns2 + 1.703 × 10−51ns3, νBLG = −0.0637 + 1.624 × 10−17ns − 6.582 × 10−34ns2 + 1.316 × 10−50ns3.

Close modal

For the kinematic viscosity ν, earlier works9,22,23 also demonstrated different ns dependence for MLG and BLG. For MLG, the viscosity has a relatively weak ns dependence, and at T = 300 K, ν ≈ 0.05 m2/s and keeps almost unvaried as ns alters.9,23 For BLG, ν rises with the increase of ns.9 In our study, we use ν = 0.05 m2/s at 300 K for MLG and calculate the BLG viscosity by fitting the temperature-converted experimental data, as shown in Fig. 1(b). We can see that when ns < 1012 cm−2, the viscosity of MLG is higher than that of BLG.

The hydrodynamic regime in graphene has been extensively investigated in previous works.8,10,24,44 In general, to ensure the device operates at the hydrodynamic (or quasi-hydrodynamic) regime, one needs at least 1/τee > max[1/τe-ph, 1/τe-imp],44 where τee, τe-ph, and τe-imp represent the electron–electron, electron–phonon, and electron–impurity scattering times, respectively. The calculations44 suggested that this condition is easier to be met in MLG at 300 K, while for BLG, the hydrodynamic window is limited to low ns and narrows with the decrease of the operating temperature, T. However, the recent experiments21 reported on the plasmonic resonance at T = 10 K and T = 77 K in a relatively large dynamic range. In our simulation, we limit the range of ns to 0.5 × 1012 cm−2 < ns < 2 × 1012 cm−2, and only consider the plasmonic detection under 300 K and 77 K (except for the mode validation section). The lower limit of ns is to prevent the effect of the distortion near the charge neutrality point (CNP), where the hydrodynamic theory could also fail.9,45 We assume that the graphene devices operating in the above parameter range fall into the hydrodynamic window.

To simulate the gated graphene plasmonic FETs, we use a one-dimensional hydrodynamic model. The governing equations consist of a continuity equation, momentum relaxation equation, and energy relaxation equation, as given below,25,46

(1)
(2)
(3)

The notations used in Eqs. (1)–(3) are summarized and explained in Table I. We use a unified charge control model (UCCM)25,47 to relate ns and U, as presented in Eq. (4). When eUKBT, the UCCM reduces to ns = CU/e,

(4)
TABLE I.

Summary of symbols used in Eqs. (1)–(3).

SymbolMeaningComment
u Hydrodynamic velocity (m/s) … 
U Gate-to-channel potential (V) U = U0 − Uch
U0: DC gate bias above threshold;
Uch: channel potential 
τ Momentum relaxation time (s) τ = μm*/e 
θ Temperature (eV) θ = kBT 
Χ Normalized heat conductivity (m2/s) χ = κ/nsκ: heat conductivity 
Cv Thermal capacitance (1) Cv = (∂Σ/∂θ)n Σ: average internal energy, Σ = θF1(ξ)/F0(ξ), ξ: chemical potential, ξ = In(exp(EF/kBT)−1), EF: Fermi energy Fk(ξ): k-order Fermi integral 
W Total energy (eV) … 
(∂W/∂t)c The collision term of ∂W/∂t (eV/s) (∂W/∂t)c = (∂Σ/∂t)c – m*u2/τ 
SymbolMeaningComment
u Hydrodynamic velocity (m/s) … 
U Gate-to-channel potential (V) U = U0 − Uch
U0: DC gate bias above threshold;
Uch: channel potential 
τ Momentum relaxation time (s) τ = μm*/e 
θ Temperature (eV) θ = kBT 
Χ Normalized heat conductivity (m2/s) χ = κ/nsκ: heat conductivity 
Cv Thermal capacitance (1) Cv = (∂Σ/∂θ)n Σ: average internal energy, Σ = θF1(ξ)/F0(ξ), ξ: chemical potential, ξ = In(exp(EF/kBT)−1), EF: Fermi energy Fk(ξ): k-order Fermi integral 
W Total energy (eV) … 
(∂W/∂t)c The collision term of ∂W/∂t (eV/s) (∂W/∂t)c = (∂Σ/∂t)c – m*u2/τ 

In regard to the boundary condition, we use the traditional open-drain condition, i.e., U(0, t) = U0 + Ua(t) and J(L, t) = 0.48,49 Here, Ua(t) is the radiation-induced small-signal voltage. For the continuous wave (CW) radiation, we assume Ua(t) = Vam cos(2πft), where Vam is the amplitude of the incident AC voltage. For the pulse detection mode, we consider the single square pulse case, and thus the incident small-signal voltage is expressed by Ua(t) = Vam(u(t) − u(t − tpw)), where u(t) is the unit step function and tpw is the pulse width. More detailed descriptions of the hydrodynamic equations and boundary conditions can be found in Refs. 25, 46, and 50.

Apart from the numerical modeling, we also use analytical theories to study the behaviors of graphene plasmonic FETs. Under the CW detection mode, the analytic theory predicts a constant DC voltage component between source and drain under the open-drain boundary condition,48,51

(5)

Here, dU is the source-to-drain voltage response and f(ω) is a frequency dependent function and is always positive. Equation (5) shows that dU is proportional to the power of incident radiation (see also Fig. 2)

FIG. 2.

Responsivity calculation scheme for continuous wave excitation. Vth is the threshold voltage and Vam is the amplitude of AC small-signal voltage.

FIG. 2.

Responsivity calculation scheme for continuous wave excitation. Vth is the threshold voltage and Vam is the amplitude of AC small-signal voltage.

Close modal

For the pulsed regime, the response performance can be evaluated by solving the linearized hydrodynamic equations in the form of U(x, t) = ∑(n)An exp(σnt)fn(x), where σn is given by25,27,28

(6)

Here, n is the odd harmonic index. If σn is real, U(x, t) will have a pure exponential decay waveform corresponding to the non-resonant regime. If σn has an imaginary part, U(x, t) behaves an oscillatory exponential decay, and the plasmonic resonance is reached. Under the first-order approximation, the response time of the plasmonic oscillation can be defined by τr = 1/Re(|σ1+|).

The hydrodynamic model was used in various previous works and showed a relatively good agreement with the experimental measurements.25,28,51–54 Here, we compare the result of our model with the experimental data of graphene plasmonic detection, as shown in Fig. 3. Figures 3(a1) and 3(a2) present the experimental detection responsivity using BLG FETs under two temperatures,9 and Figs. 3(b1) and 3(b2) illustrate the corresponding simulation results under similar operating conditions. As shown in Fig. 3(a1), at 10 K, f = 0.13 THz a relatively smooth Ra curve is observed, and the absolute amplitude of Ra reduces with rising U0. This is a typical broadband (non-resonant) operation performance. In Fig. 3(b1), where simulation curves are given, we can see that the simulated responsivity at 0.13 THz has a similar trend as the experimental data, and the order of magnitude of Ra in these two figures is the same. When the incident frequency rises to 2 THz, the experimental response curve becomes rugged, reflecting various resonant peaks. The same feature can be observed in the simulated Ra curve shown in Fig. 3(b1), and the positions of resonant peaks are very close to the 2 THz experimental curve. This indicates that our hydrodynamic model can fairly reproduce the THz detection response. Similar conformity is also obtained at 77 K, as shown in Figs. 3(a2) and 3(b2). Those results suggested the qualitative validity of the hydrodynamic model in analyzing the graphene-based plasmonic THz detection problems.

FIG. 3.

Experimental data [(a1) and (a2)] vs the modeling results [(b1) and (b2)]. The experimental data are extracted from Ref. 21. The operating conditions are L = 3–6 μm, μ ≈ 10 m2/V s for T = 10 K and μ ≈ 8 m2/V s for T = 77 K; the effective plasmon lifetime,21τp ≈ 0.3–0.9 ps; barrier layer thickness db = 80 nm, made with hBN. The parameters used in simulation are L = 5.1 μm, τp = 0.8 ps for T = 10 K and τp = 0.4 ps at T = 77 K; barrier layer: db = 80 nm, ɛr = 3.8; viscosity ν = 0.1 m2/s. The responsivity Ra is calculated through Ra = dU/P, where dU is the source-to-drain DC voltage and P is the incident radiation power.

FIG. 3.

Experimental data [(a1) and (a2)] vs the modeling results [(b1) and (b2)]. The experimental data are extracted from Ref. 21. The operating conditions are L = 3–6 μm, μ ≈ 10 m2/V s for T = 10 K and μ ≈ 8 m2/V s for T = 77 K; the effective plasmon lifetime,21τp ≈ 0.3–0.9 ps; barrier layer thickness db = 80 nm, made with hBN. The parameters used in simulation are L = 5.1 μm, τp = 0.8 ps for T = 10 K and τp = 0.4 ps at T = 77 K; barrier layer: db = 80 nm, ɛr = 3.8; viscosity ν = 0.1 m2/s. The responsivity Ra is calculated through Ra = dU/P, where dU is the source-to-drain DC voltage and P is the incident radiation power.

Close modal

It is worth noting that the resonant peaks in Fig. 3 are relatively broad and weak. This corresponds to a broadening effect of viscosity proposed in previous papers.25,26 The resonant peaks might become sharper and more distinguishable with the viscosity reduction and/or an increase of the channel length.

Figure 4 presents the normalized voltage response (R) of graphene plasmonic FETs as functions of radiation frequency f and gate bias U0 under the continuous wave detection mode. The normalization is done by R = dUU0/Vam2, where dU is the absolute source-to-drain DC voltage component and Vam is the amplitude of the incident AC voltage. As seen, the amplitude of R is in the order of 10−3 ∼ 1. Compared to our previous results,29 the voltage response level of graphene plasmonic detector is lower than that of Si, III–V, and diamond devices. This is because graphene always has a small effective mass, and the mobility values we used are not extradentary. In high mobility samples, the detection sensitivity could be enhanced. For example, if the mobility is elevated 10 times, the peak R would reach ∼101, which is higher than the peak R of Si and III–V plasmonic FETs but still lower than diamond devices. Besides, the simulated response data slightly deviate from the analytical curve, an effect of high viscosity.25,29 Due to a larger viscosity, the deviation in MLG is larger than that of BLG. Those results indicate that graphene plasmonic FET has no obvious advantage as a CW THz detector compared to FETs fabricated with other materials.

FIG. 4.

Normalized voltage response (R) of MLG and BLG plasmonic FETs as functions of f and U0. The operating conditions are L = 130 nm, T = 300 K, Vam = 5 mV, dg = 50 nm, ɛr = 3.8. In (b), U0 begins with 1 V to avoid being too close to the CNP.

FIG. 4.

Normalized voltage response (R) of MLG and BLG plasmonic FETs as functions of f and U0. The operating conditions are L = 130 nm, T = 300 K, Vam = 5 mV, dg = 50 nm, ɛr = 3.8. In (b), U0 begins with 1 V to avoid being too close to the CNP.

Close modal

Now, we evaluate the detection performance of graphene in the pulsed regime. Here, we consider the single square pulse condition. Figure 5 illustrates the response time (τr) of MLG and BLG FETs vs the incident pulses width (tpw) at T = 300 K and T = 77 K. As seen, the variation tendency of τr in graphene is identical to that in Si, III–V, and diamond materials in our previous paper.30 That is, under the short pulse condition (tpwL/s), the response time is relatively short and almost independent of tpw. As tpw increases and approaches L/s, τr starts to increase, and then stabilizes when reaching the long pulse mode (tpwL/s). It is worth noting that under the operating condition given in Fig. 5, the system always operates at the plasmonic resonant mode (the ballistic mode). The plasma wave travels through the channel, gets reflected, and decays with time due to friction and viscosity, thus generating an oscillatory decay voltage at the drain.27,28,30 The response time in this mode can be expressed by τr = 2τ/(1 + π2ντ/4L2),27 and τr ≈ 2τ under low viscosity conditions. The analytical response expression is valid at the long pulse mode, while in the short pulse case, the response time is reduced to approximately τr(L/2)0.5.30 From Fig. 5, we can see that the response time at tpwL/s is significantly lower than 2τ, which indicates a strong viscosity effect. Besides, the BLG response time is longer than that of MLG due to a larger effective mass. More importantly, due to the small effective mass and high viscosity, the pulse response time in graphene is much smaller than the response time of Si, III–V, and diamond materials (∼0.1–1 ps).30 For higher mobility samples, the response time of graphene plasmonic FETs will be elevated, but we can still maintain a relatively short response time in a large mobility range (e.g., μ < ∼ 2 m2/V s). This suggests that the graphene plasmonic FET might be more suitable as a rapid femtosecond pulse detector than plasmonic FETs fabricated using other materials. When T drops to 77 K, the graphene response time reduces, as shown in Fig. 5(b). This is mainly due to a significant increase in viscosity. Besides, the long pulse response time deviates further from the 2τ limit at 77 K.

FIG. 5.

Simulation results of response time vs the pulse width for MLG and BLG plasmonic FETs under (a) 300 K and (b) 77 K. The horizontal dashed arrow lines illustrate the 2τ limit, and the dotted vertical arrow lines highlight the position of characteristic time L/s. The mobility (a) 0.30 m2/V s for MLG and 0.20 m2/V s for BLG at 300 K, (b) 0.39 m2/V s for MLG and 0.17 m2/V s for BLG at 77 K. The viscosity (a) 0.05 m2/s for MLG and 0.034 m2/s for BLG at 300 K, (b) 0.384 m2/s for MLG and 0.263 m2/s for BLG at 77 K.

FIG. 5.

Simulation results of response time vs the pulse width for MLG and BLG plasmonic FETs under (a) 300 K and (b) 77 K. The horizontal dashed arrow lines illustrate the 2τ limit, and the dotted vertical arrow lines highlight the position of characteristic time L/s. The mobility (a) 0.30 m2/V s for MLG and 0.20 m2/V s for BLG at 300 K, (b) 0.39 m2/V s for MLG and 0.17 m2/V s for BLG at 77 K. The viscosity (a) 0.05 m2/s for MLG and 0.034 m2/s for BLG at 300 K, (b) 0.384 m2/s for MLG and 0.263 m2/s for BLG at 77 K.

Close modal

As seen from Fig. 5, the response performance of graphene FETs is highly affected by the viscosity. Since the above cases correspond to the resonant detection mode, we further study the detection properties under other regimes and further explore the viscosity effects. Figure 6 presents the response time as a function of carrier mobility with different feature sizes, taking BLG as the example. By varying the mobility, the plasmonic FETs can be driven into different operating regimes.

FIG. 6.

Response time vs mobility μ for BLG plasmonic FETs with different channel lengths. The symbols represent the simulation values, and the solid lines are the analytic curves. The operating parameters are U0 = 2 V, ν = 0.034 m2/s, T = 300 K.

FIG. 6.

Response time vs mobility μ for BLG plasmonic FETs with different channel lengths. The symbols represent the simulation values, and the solid lines are the analytic curves. The operating parameters are U0 = 2 V, ν = 0.034 m2/s, T = 300 K.

Close modal

When L > 7 nm, the τr curves demonstrate three distinct regions: the non-resonant (collision dominated) region, the ballistic region, and the viscous region.27,28 At a low mobility (i.e. μ < μTR, where μTR is a transition mobility), the plasma wave is non-exist and the device operates in the non-resonant mode. In this mode, the carrier transport is dominated by collisions with phonons and/or impurities, and the temporal voltage response is a pure exponential decay.27 Once the mobility reaches the critical value, μTR, the plasma waves are excited, and the device goes into the resonant mode. The transition mobility μTR is given by μTR = (Lems)/(1 − πν/4Ls), which is obtained by letting the square root term of σ1+ to be zero [see Eq. (6)]. Under the resonant condition, if the mobility is not very high, or π2ντ/4L21, we have τr ≈ 2τ.27 We call this region the ballistic region since the electron–electron scattering takes over but is still not strong enough to induce the viscous behavior. If the mobility is very large so that π2ντ/4L21, τr ≈ 8L22ν, which is associated with ν but independent of μ. Then, the plasmonic FET enters the viscous regime.

From Fig. 6, we find that the ranges of those three regions vary with L. As L decreases from 250 nm to 14 nm, the critical mobility μTR decreases, and the boundary of the viscous region moves leftward. Thus, the range of the viscous region expands while the band of ballistic region shrinks. As expected, the viscosity effect becomes more significant as L scales down. When L decreases to 7 nm, the response performance of graphene FETs changes dramatically. As seen in Fig. 6, the response time at L = 7 nm decreases monotonically with the increase of μ and gradually saturates at large μ. The simulation result also reveals a very different response profile. Figure 7 compares the temporal voltage response waveform at L = 32 nm and L = 7 nm. As seen in Fig. 7(a), when L = 32 nm, the response waveform turns from an exponential decay (olive curve) to a quasi-sinusoidal oscillatory decay (blue, magenta, and dashed red curves) as μ increases, suggesting the transition from the non-resonant mode to the resonant mode. In the case of L = 7 nm, however, the oscillatory decay does not show up even at very high mobilities. Instead, the voltage response turns from negative to positive in few femtoseconds and decays quasi-exponentially, exhibiting non-resonant features. The distorted temporal waveform makes us hard to calculate the response time, but we do observe the convergence of the response waveform at high mobilities, corresponding to the saturation of τr in the analytical curve shown in Fig. 6.

FIG. 7.

Temporal source-to-drain voltage response of BLG plasmonic FETs at (a) L = 32 nm and (b) L = 7 nm under four different mobility values.

FIG. 7.

Temporal source-to-drain voltage response of BLG plasmonic FETs at (a) L = 32 nm and (b) L = 7 nm under four different mobility values.

Close modal

The results in Figs. 6 and 7 revealed another non-resonant window at a very low channel length. To evaluate this issue in a more systematic manner, we focus on the linearized analytic theory. Note that the existence of the resonance is determined by the square root term f(L, τ, s, n) in Eq. (6),

(7)

Using the first-order approximation and defining

(8)

we can see that f1 determines the polarity of the square root term in σ1+. Solving f1 < 0 (to ensure that σ1+ has an imaginary part) in terms of μ yields μ = (Lems)/(1 − πν/4Ls), which is the definition of μTR.

We now evaluate f1 < 0 in terms of L. Taking x = 1/L as the unknown, the roots of equation f1 = 0 are

(9)

or, equivalently,

(10)

The solution of f1 < 0 will be discussed under the following conditions:

  1. when s2 > ν/τ, L1 and L2 are real. To ensure f1 < 0, we need L2 < L < L1. Therefore, the range of L for resonant operation is bounded at a given μ. The ΔL range is given by
    (11)

We can see that ΔL increases with rising τ, s and decreases with the increase of ν.

When τ (or μ) is very large, L1, L2, and ΔL converge to

(12)

That is, the upper limit limτL1=πsτ rises with rising μ, while the lower limit limτL2 is a fixed value independent of μ. This indicates that when L is very low, the plasmonic FETs would always operate in non-resonant mode, regardless of the mobility. Also, the upper limit πsτ is in fact equivalent to the boundary for broadband detection (sτ/L1) proposed in previous papers.48 This means that the plasma oscillation generated near the source side cannot reach the drain side due to a long channel. It is also noted that the lower limit L = πν/4s is a pole in the expression of μTR. With a relatively large viscosity, this lower limit of L in graphene is larger than that in other traditional materials. Hence, it is easier to achieve the mode conversion by scaling in graphene.

  1. when s2 < ν/τ, or ν > s2τ ≈ μU0, we have f1 > 0. This means at a given mobility, there exists a critical viscosity νNR ≈ μU0 so that when ν > νNR, the plasmonic FET cannot reach the resonance mode, regardless of the channel length. Under this circumstance, Re[σ1+] = σ1+, so the response time can be expressed by
    (13)

This expression is valid for all non-resonant cases. When L = >0, τr = >ν/s2. At large L, τr4L2π2s2τ+νs2, i.e., the response time rises quadratically with the increase of L.

To evaluate the validity of the above theory, Fig. 8 compares the simulation and analytic results of τr for BLG plasmonic FETs as a function of L. As seen, at low viscosity (ν < νNR), the resonant band can be observed in the analytic curve, and the simulation values agree well with the analytic results. With the increase of viscosity, the resonant band narrows, as predicted by Eq. (12). When ν exceeds νNR, the resonant band disappears, and the system operates at a fully non-resonant regime. The simulation data exhibit a good agreement with the analytic curves for relatively large L cases. When L < 100 nm, the modeled τr values drop below the analytic curve and approach 0 when L < 20 nm, indicating the failure of analytic theory. From the simulation, we noticed that the plasma wave velocity s under L < 100 nm is higher than the theoretical value. Therefore, the decrease of response time at low L might be caused by the increased s and thus reduced ν/s2. The speed-up of the plasma wave here could be related to the viscosity effect. A more in-depth mechanism of this phenomenon is still missing and requires further investigation. In the design of plasmonic FETs, we may use this phenomenon to further shorten the response time and accelerate the device response.

FIG. 8.

Response time vs L for different viscosity values for BLG FETs at U0 = 2 V, tpw = 10−11 s. Simulation values are presented by symbols, and the analytic results are given by solid curves. The critical viscosity νNR = 0.392 m2/s. The dashed circles highlight the boundaries of non-resonant/resonant regions.

FIG. 8.

Response time vs L for different viscosity values for BLG FETs at U0 = 2 V, tpw = 10−11 s. Simulation values are presented by symbols, and the analytic results are given by solid curves. The critical viscosity νNR = 0.392 m2/s. The dashed circles highlight the boundaries of non-resonant/resonant regions.

Close modal

Figure 9 shows high viscosity BLG FET (ν = 0.5 m2/s) at different mobilities. As before, the simulated response time data agree with the analytic curves except those at the short channel region. When the mobility rises, the system can be driven out of fully non-resonant mode (since νNR = μU0 rises). However, the lower resonant boundary cannot cross the limit L = πν/4s, since it is independent of μ.

FIG. 9.

Response time vs L at different mobilities for BLG FETs under U0 = 2 V, tpw = 10−11 s, ν = 0.5 m2/s > νNR. The dashed line highlights the position of L = πν/4s.

FIG. 9.

Response time vs L at different mobilities for BLG FETs under U0 = 2 V, tpw = 10−11 s, ν = 0.5 m2/s > νNR. The dashed line highlights the position of L = πν/4s.

Close modal

Now, we evaluate the boundary of the viscous region. As mentioned earlier, to ensure the domination of the viscosity effect, we need, from Eq. (6),

(14)

where νcr is a characteristic viscosity. For ννcr , the loss is dictated by scattering; for ννcr, the loss is determined by viscosity (viscous regime). Rewriting this inequality into the following form:

(15)

We obtain μTν, the approximate mobility boundary of the viscous regime. Apparently, μTν drops with the decrease of L, suggesting the leftward expansion of the viscous region. This confirms our observation in Fig. 6. In general, μTνμTR, but when L is very low, μTν < μTR, and from this inequality, we obtain

(16)

It can be seen that the characteristic length Lcr ≈ πν/4s, which is exactly the lower boundary of the resonant region. This result indicates that in a short channel device, the carrier transport is dominated by the viscosity. One possible reason is that the mean free path of electron–phonon scattering or electron–impurity scattering becomes comparable or even larger than the channel length under this condition, and thus these scattering rates are restricted and viscosity takes over. With a strong viscosity and a short channel, the carriers cannot reach the resonant oscillation.

Figure 10 summarizes the variation of operating regimes in a Lν scale. As seen, the viscous regime penetrates into both resonant and non-resonant modes, suggesting the significant role of viscosity in the graphene plasmonic detection.

FIG. 10.

Schematic of operating regimes in a graphene plasmonic FET.

FIG. 10.

Schematic of operating regimes in a graphene plasmonic FET.

Close modal

Table II shows the typical material parameters and L1, L2, ΔL, and νNR for graphene, Si, GaN, InGaAs, and diamond materials. As seen, the MLG and BLG have relatively large L2 and relatively small L1 values compared to those of other materials. Note that the mobility and viscosity of graphene are adjustable in a large dynamic range, thus L1, L2, ΔL, and νNR can also be adjusted by changing μ and ν. For example, in a high viscosity sample, the lower limit L1 can increase to ∼100 nm, as shown in Fig. 9, given a large mobility sample, the upper limit L could rise to several μm. This shows that graphene has a much better mode tunability compared to other materials.

TABLE II.

Material parameters and L1, L2, ΔL, νNR in for different materials. Note: the material parameters are taken from Refs. 31–33 and 36–39 (MLG and BLG); Refs. 55–58 (Si); Refs. 58–60 (GaN); Refs. 27, 61, and 62 (InGaAs); and Refs. 63–66 (p- and n-diamond).

MaterialsU0 (V)μ(m2/V s)ν (m2/s)m*/m0s (m/s)τ (fs)L2 (nm)L1 (nm)ΔL (nm)νNR (m2/s)
MLG 0.3 0.05 0.017 4.54 × 106 29.17 8.85 406.8 397.9 0.6 
BLG 0.2 0.034 0.036 3.13 × 106 39.92 8.79 383.2 374.4 0.4 
Si 0.1 2.35 × 10−4 0.19 1.36 × 106 10.80 0.14 461.7 461.5 0.2 
GaN 0.2 1.47 × 10−3 0.23 1.24 × 106 26.16 0.93 1015.3 1014.3 0.4 
InGaAs 0.04 0.041 2.93 × 106 23.32 10.78 2134.5 2123.7 2.0 
p-diamond 0.3 1.6 × 10−4 0.663 7.28 × 105 11.31 0.17 2587.9 2587.7 0.6 
n-diamond 0.5 5.17 × 10−4 0.36 9.88 × 105 10.24 0.41 3178.0 3177.6 1.0 
MaterialsU0 (V)μ(m2/V s)ν (m2/s)m*/m0s (m/s)τ (fs)L2 (nm)L1 (nm)ΔL (nm)νNR (m2/s)
MLG 0.3 0.05 0.017 4.54 × 106 29.17 8.85 406.8 397.9 0.6 
BLG 0.2 0.034 0.036 3.13 × 106 39.92 8.79 383.2 374.4 0.4 
Si 0.1 2.35 × 10−4 0.19 1.36 × 106 10.80 0.14 461.7 461.5 0.2 
GaN 0.2 1.47 × 10−3 0.23 1.24 × 106 26.16 0.93 1015.3 1014.3 0.4 
InGaAs 0.04 0.041 2.93 × 106 23.32 10.78 2134.5 2123.7 2.0 
p-diamond 0.3 1.6 × 10−4 0.663 7.28 × 105 11.31 0.17 2587.9 2587.7 0.6 
n-diamond 0.5 5.17 × 10−4 0.36 9.88 × 105 10.24 0.41 3178.0 3177.6 1.0 

As reported in our previous paper,30 the viscosity of the plasmonic FET material can be extracted using τr = 2τ/(1 + π2ντ/4L2) in the resonant mode. That is, by plotting τr−1 vs L2 and getting ν from the slope of the curve (since 1/τr = 1/2τ + π2ν/8L2). Now, we discuss the viscosity extraction in the non-resonant mode. For s2 > ν/τ, the analytic expression of τr is given by Eq. (13). This equation predicts that when L = > 0, τr = > ν/s2. However, simulation results in Figs. 8 and 9 show that the analytic expression is invalid at low L. Since the region where the analytic theory fails begins at around L =  (∼125 nm in our BLG FET case), and the analytic curve of τr becomes very flat in this region, we could assume τr(L = ) ≈ ν/s2, and, therefore, ν ≈ s2τr(L = ). A more rigorous method is to fit the experimental data under relatively large L. The fitting curve follows Eq. (13) given by

(17)

Here, C1 = 1/π2s2τ, C2 = 1/4s2, and C3 = 1/π2s2. To obtain C1, C2, and C3, we need to know μ (τ = τm/e) and s. The plasma velocity s can be obtained from the delay time data.

Figure 11 shows the fitting results of simulation data for BLG FETs under ν = 0.5 m2/s and ν = 0.8 m2/s using Eq. (17). As seen, the fitted curves exhibit a good agreement with the analytical curves given in Fig. 8. The fitting yields ν = 0.724 m2/s for ν = 0.8 m2/s case and ν = 0.445 m2/s for ν = 0.5 m2/s case, suggesting that this method tends to underestimate the viscosity. Nevertheless, it still provides a relatively high accuracy for viscosity extraction. Compared to the resonant viscosity extraction method proposed earlier,30 this non-resonant method demonstrates a higher accuracy, possibly because of a higher polynomial order of the fitting function. We could use this method to evaluate the temperature dependence of viscosity in graphene.

FIG. 11.

Simulation points and fitting curves [following Eq. (17)] of response time for BLG FETs under ν = 0.5 m2/s and ν = 0.8 m2/s.

FIG. 11.

Simulation points and fitting curves [following Eq. (17)] of response time for BLG FETs under ν = 0.5 m2/s and ν = 0.8 m2/s.

Close modal

THz continuous wave (CW) detection and ultrashort pulse detection by monolayer graphene (MLG) and bilayer graphene (BLG) FETs were studied by a validated hydrodynamic model and compared with the analytical theory and experimental data. The simulation revealed a much more important role of viscosity in graphene compared to more traditional semiconductor materials. Graphene response time to short excitation pulses could be much smaller than that of Si, GaN, InGaAs, or diamond FETs. Therefore, graphene and bilayer graphene FETs could be used as femtosecond pulse detectors. At relatively low viscosities, the resonant window in graphene plasmonic FETs were found to be limited in a certain channel length range, and this range shrunk with the increase to viscosity. As a sufficient large viscosity, the resonant window disappeared, and the device would always operate on the non-resonant, viscous regime. We developed the analytical expression of response time in this regime, and it demonstrated a good agreement with the simulation data. This expression could be also used for the graphene parameter extraction including the electron and hole viscosity measurements.

This work was supported by the U.S. Air Force Office of Scientific Research (No. FA9550-19-1-0355) (Project Manager Dr. Ken Goretta), Army Research Office (No. W911NF-17-S-0002) (Project Manager Dr. John Qiu), and the Army Research Laboratory under ARL MSME Alliance (Project Manager Dr. Meredith Reed).

The data that support the findings of this study are available from the authors upon reasonable request.

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