T the fact that it really is flying by way of a cavity. We are going to show that the regimes exactly where 1 finds Unruh effect in cavities (defined as thermalization from the probe to a temperature proportional to its acceleration when interacting using the vacuum) are precisely those regimes where the probe can not resolve information about the impact from the cavity walls. In summary, we are going to show that you will find regimes where the probe is blind towards the fact that it truly is in a cavity and so experiences thermalization as outlined by Unruh’s law.Symmetry 2021, 13,III. OUR show that is certainly flying via a cavity. We willSETUP the regimes DeWitt interCAY10502 site action Hamiltonian [ where a single finds Unruh effect in cavities (defined as therIV. NON-PERTURBATIVE ^ ^ Think about a probe to a temperature proportional to malization of theprobe that is initially co-moving with all the HI = qp (t( ^ cavity wall at x = interacting using the vacuum) are a 0 and after that begins to accelerate at its acceleration when of probe’s d subsequent coupling strength. T continuous price a 0 where the far end of your cavity precisely those regimes towardsthe probe cannot resolve at whereWeis the compute 4the20 In interaction picture the tim x = L 0. Within the effect of probe’s correct time, , this tures the fundamental characteristics of th details about terms of your the cavity walls. the probe-field method inside the n m action when exchange of angular th portion of your will show is provided by In summary, wetrajectory that there are regimes where evant [ ]. Note that x( the probe is blind towards the truth that it is actually in a cavity and so 3. Our Setup c2 -i nmax experiences thermalization – 1), t( to= c sinh(a /c), (5) by Eq. (five) while the probe accelera according ) Unruh’s law. ^x x = (cosh(a /c) that is initially co-moving together with the cavity wall at n = T and then U I = 0 expin the second Consider a probe cavity. The trajectory a a (n-1) starts to accelerate at a continuous price a 0 towards the far a simple reversed-translati finish with the cavity at x = L 0. -1 c 2 for In terms the probe’s correct time, , this portion cavity0 of max = a cosh SETUP The in the trajectory is provided by III. OUR (1 + aL/c ). The probe’s reduced dynamics is crossing time in the lab frame is tmax = L 1 + 2c2 /aL. c two c The probe exits which )cavity at some speed, t(the c IV. NON-PERTURBATIVE pTI I [^p ] = Tr (Un (^ x ( initially co-moving with , rela(five) ^ I Take into account a probethe firstis = (cosh( a/c) – 1),vmax ) = sinh( a/c), n a maximum Lorentz aspect a tive for the x cavity walls with cavity wall at the= 0 and after that begins to accelerate at a max price a 0 towards + 1 far 2 . two We subsequent compute instances n constant=0cosh(amax /c) c= 1theaL/cend of).the cavity at for max = a cosh- (1 + aL/c The cavity-crossingComposing the frame is = dyn time within the lab the probe’s 1 a At 0. Inmax the 2probe probe’sthe second cavitythisthe Inside the interaction picture the time-e = enters appropriate time, , of probe BRD0209 Epigenetics accelerates and decelerat x = L t = L terms with the The probe exits the very first cavity at some speed, vmax , relative to 1 max two-cavityc cell+ 2c /aL. and begins decelerating with probe-field program in the nth up portion ofcavity walls withis given byLorentz element correct ac- thebuild )the1 interaction image ca the trajectory maximum the max = cosh max /c + aL/c2 celeration a. The probe reaches the far end in the second ( acell, I= = I .I . 1,two cell 2 At = the and 1 starts two cavity,cx =2L, max theit comes to rest at = 2max . of your two-cavity just as probe enters c s.

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