2017
DOI: 10.1038/s41598-017-14125-1
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Radiation-induced resistance oscillations in 2D electron systems with strong Rashba coupling

Abstract: We present a theoretical study on the effect of radiation on the mangetoresistance of two-dimensional electron systems with strong Rashba spint-orbit coupling. We want to study the interplay between two well-known effects in these electron systems: the radiation-induced resistance oscillations and the typical beating pattern of systems with intense Rashba interaction. We analytically derive an exact solution for the electron wave function corresponding to a total Hamiltonian with Rashba and radiation terms. We… Show more

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Cited by 13 publications
(20 citation statements)
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“…With the expression of X ( t ) (Equation ) and according to the radiation‐driven electron orbit model, we obtain for the average distance advanced by the electron in a scattering event centerΔX(t)=ΔX0eγ2τA[sin ω+τ+sin ωτ]center=ΔX02Aeγ2τsin ωτ cosnormalλτ where we have used the well‐known expression: sintrue(θ1true)+sintrue(θ2true)=2sintrue[θ1+θ22true]costrue[θ1θ22true] and we have considered that AB and that ω±ω±λ. The time, τ, according to the radiation driven electron orbit model, is the “flight time,” the time it takes the electron to jump due to scattering from one orbit to another and its value is given by τ=2πωc. Finally and following the radiation‐driven electron orbit model we end up with an expression for R xx : RxxΔX02Aeπγwcsintrue(2πωωctrue)costrue(2…”
Section: Theoretical Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…With the expression of X ( t ) (Equation ) and according to the radiation‐driven electron orbit model, we obtain for the average distance advanced by the electron in a scattering event centerΔX(t)=ΔX0eγ2τA[sin ω+τ+sin ωτ]center=ΔX02Aeγ2τsin ωτ cosnormalλτ where we have used the well‐known expression: sintrue(θ1true)+sintrue(θ2true)=2sintrue[θ1+θ22true]costrue[θ1θ22true] and we have considered that AB and that ω±ω±λ. The time, τ, according to the radiation driven electron orbit model, is the “flight time,” the time it takes the electron to jump due to scattering from one orbit to another and its value is given by τ=2πωc. Finally and following the radiation‐driven electron orbit model we end up with an expression for R xx : RxxΔX02Aeπγwcsintrue(2πωωctrue)costrue(2…”
Section: Theoretical Modelmentioning
confidence: 99%
“…The time, τ, according to the radiation driven electron orbit model, is the “flight time,” the time it takes the electron to jump due to scattering from one orbit to another and its value is given by τ=2πωc. Finally and following the radiation‐driven electron orbit model we end up with an expression for R xx : RxxΔX02Aeπγwcsintrue(2πωωctrue)costrue(2πλωctrue) …”
Section: Theoretical Modelmentioning
confidence: 99%
“…The phase difference α can be left out with the appropriate time shift (all driven-LS are oscillating in phase). And the total electronic orbit center coordinate in the x-direction, X ( t ), changes according to our model by 29 …”
Section: Theoretical Modelmentioning
confidence: 99%
“…Following the radiation-driven electron orbit model we can obtain the advanced distance by the electron due to charged impurity scattering when jumping between irradiated LS 29 :where Δ X (0) is the shift of the guiding center coordinate for the eigenstates involved in the scattering event when there is no light. According to the radiation-driven electron orbit model, the time is the flight time or the time it takes the electron to jump from a Landau state to another one due to scattering.…”
Section: Theoretical Modelmentioning
confidence: 99%
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