2016
DOI: 10.1209/0295-5075/113/57004
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Evidence of radiation-driven Landau states in 2D electron systems: Magnetoresistance oscillations phase shift

Abstract: -We provide the ultimate explanation of one of the core features of microwave-induced magnetoresistance oscillations in high mobility two dimensional electron systems: the 1/4-cycle phase shift of minima. We start with the radiation-driven electron orbits model with the novel concept of scattering flight-time between Landau states. We calculate the extrema and nodes positions obtaining an exact coincidence with the experimental ones. The main finding is that the physical origin of the phase shift is a delay of… Show more

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Cited by 9 publications
(6 citation statements)
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“…where we have considered that the amplitudes of both modes are similar, i.e., A ≃ B and that w ± ≃ w ± λ. The time, τ , according to the radiation driven electron orbit model 58,59 , 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 = 2π wc . Following the same RIRO model and using the obtained ∆X(t), we end up with an expression for R xx 58,59 :…”
mentioning
confidence: 99%
“…where we have considered that the amplitudes of both modes are similar, i.e., A ≃ B and that w ± ≃ w ± λ. The time, τ , according to the radiation driven electron orbit model 58,59 , 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 = 2π wc . Following the same RIRO model and using the obtained ∆X(t), we end up with an expression for R xx 58,59 :…”
mentioning
confidence: 99%
“…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%
“…If now we switch on radiation, first of all we have to add to the Hamiltonian H 0 a radiation term H R and then: H 0 = ( H B + H SO + H R ), where ε 0 being the radiation electric field and w the corresponding radiation frequency. H 0 can again be solved exactly 20 , 21 , 51 , 52 , and the solution for the electronic wave function is made up, as above, of two states branches. The wave function for the + branch is, and for the - branch, where, as above, Φ n is the solution for the Schrödinger equation of the unforced quantum harmonic oscillator where x cl ( t ) is the classical solution of a forced harmonic oscillator 20 , 51 , 52 , where e is the magnitude of the electron charge and γ is a phenomenologically introduced damping factor for the electronic interaction with acoustic phonons.…”
Section: Theoretical Modelmentioning
confidence: 99%