arXiv:astro-ph/0008480v1 30 Aug 2000 eoe rud18 anyb lnfr ¨ng (1979), K¨onigl & Blandford by was mainly jets 1980 relativistic around in veloped emission synchrotron of theory The Introduction 1. oeln 0yaso ycrto aigi h e f3 273 3C of jet the T¨urlerM. in flaring synchrotron of years 20 Modelling orsodneto Correspondence 1 2 ie–glxe:jt usr:idvda:3 7 ai co radio – 273 3C individual: galaxies quasars: tinuum: – jets galaxies: – tive words: Key line-of-sight. the from away bends di with and/or decelerates material emitting alterna do synchrotron or, radius the jet that the jet down the distance with that rath linearly evidence is increase not some front also shock for is the suggest, There behind results turbulent. field The magnetic the jet. that the cons stance, of to properties able physical are the light-curves submillimetre-to-rad different 5000 the superlu than in apparently observations more with The jet velocities. the minal along move distin to the observed to out linked tures physically the Gear are that light-curves & idea the in Marscher the seen reinforces of 273 also model it 3C shock Indirectly, the of (1985). to curves support light strong submillimetre-to-radio gives the of shapes confront closely properties so variability is quasar. multi-wavelength model long-term a that the time to first the distinct is seventeen of It series bursts. a in 273 lo 3C thirteen of light-curves simultaneously term decompose to behind individua average able of just the are peculiarities we of region bursts, the parameterization small of proper and a evolution a in outburst’s By material front. t jet shock expected the the is which by outburst emitted synchrotron be a define a model in of The wave, properties jet. the shock able non-adiabatic decelerating now and or is non-conical origin which curved, accelerating the (1985), of an the Gear generalization describe & a to of Marscher is of variations It model 27 years. observed shock 3C 20 quasar last the the bright during well the of reproduce emission to submillimetre-to-radio able is Abstract. 2000 July 5 Accepted / 2000 March 2 Received edofrn eussto requests offprint Send 30.85 10.;1.01 11. C23 13.18.1) 273; 3C 11.17.4 11.10.1; 11.01.2; 03(02.18.5; are: codes thesaurus Your later) hand by inserted be (will no. manuscript A&A eeaOsraoy h e alets5,C-20Sauvern CH-1290 51, Maillettes des ch. Observatory, Geneva INTEGRAL h blt ftemdlt erdc h eydifferent very the reproduce to model the of ability The 1 epeetapeoeooia e oe which model jet phenomenological a present We , 2 aito ehnss o-hra aais ac- galaxies: – non-thermal mechanisms: radiation cec aaCnr,c.d’ ch. Centre, Data Science ..L Courvoisier T.J.-L. , [email protected] : .T¨urler (ISDC) M. : 1 , 2 n .Paltani S. and , cga1,C-20Vrox Switzerland Versoix, CH-1290 16, Ecogia ´ 1 , 2 stance fea- ct tively, bursts out- l ,Switzerland y, train fa of out- ng- de- in- ed es n- er io al o 3 s - 98 ol olwteeryeouino igesynchrotro 0420 single 1996 PKS of 279, (1995, evolution 3C al. in early et outbursts the Stevens follow and could (1995) 1998) al. co et be Litchfield to o assumed allowed stant, synchrotron spectrum quiescent individual sources a of subtracting few By evolution bursts. a spectral the of study light-curves to radio and millimetre 140. NRAO illustr quasar as the spectrum, for total (1988) flat Marscher nearly by the a model in form features shock to distinct the overlap all often constrain of emission to the use because to MG85, difficult of be to measurement found flux inte were baseline total long Multi-wavelength disti very (VLBI). the using ferometry higher observed for jet at explanation the neglected simple in components be a cannot provides which It frequencies. electrons, energ inverse-Compton the and of in- synchrotron losses to of advantage effects the however the has clude et MG85 (Hughes of Lacertae model Hughes The BL den 1989b). of of flux and variability low-frequency code the polarization angle describe computer and opening to sity The able constant was adiabatic. of (1989a) is al. cone et flow that a jet propagat- assumed to the wave groups confined that shock Both is jet. a jet relativistic of the simple pro- emission a (1985) the down al. for ing et model Hughes a and posed MG85) hereafter & (1985, Marscher both Gear 1985, In K¨onigl (1981). and (1980) Marscher al,te“yrdapoc”o ¨re 20)mdl stric models (2000) T¨urler of approach” spectrum. “hybrid synchrotron flaring the the nally, describ of (1992), evolution shock al. et the Valtaoja three-stage or directly MG85 on differ of based those at like approach outbursts models, second individual of A th light-curves frequencies. empirically the ap- describes of “light-curve and shape called model-independent so The is frequency. proach” and ev time these of evolution both the with describe to I Paper appro in different presented Two are events. flaring self-similar of comple series a a in light-curve multi-wavelength consists long-term which of decomposition prop- outbursts, observed synchrotron the derive of to erties approach new a proposed I) Paper onse the until one. outburst next t an the because of evolution mainly the strongly, follow it only could constrain MG to the failed to but support model, additional gave studies These spectively. ti nysne19 httevr elsmldttlflux total sampled well very the that 1995 since only is It ooecm hspolm ¨re ta.(99,hereafter (1999b, al. et T¨urler problem, this overcome To − 1,3 4 n C23 re- 273, 3C and 345 3C 014, ASTROPHYSICS ASTRONOMY oebr8 2018 8, November AND aches into s ated ents hey of t nct ent Fi- ut- tly 85 jet al. n- es te r- y n e s - , 2 M. T¨urler et al.: Modelling 20 years of synchrotron flaring in the jet of 3C 273 the shape of the synchrotron spectrum, but leaves the evolution these fluxes as a free parameter of our fit.1 To smooth out the of the spectral turnover as free as possible. The results of this dips in the GBI light-curves (cf. T¨urler et al. 1999a), we aver- third approach, based on self-similar outbursts as in Paper I, age all GBI observations into bins of 10 days. Finally, we do were found to be in very good agreement with the spectral evo- not consider the GBI measurements before1980,to avoid a flux lution expected by the shock model of MG85. increase in the light-curve due to an outburst that started before After this last test, the next step, which is presented here, is 1979. We end up with a total of 5234 observational points to to adapt the shock model of MG85 in order to describe physi- constrain the shock model. cally both the average evolution of the outbursts and their indi- vidual specificity. This generalized shock model, described in Sect. 3, takes into account the effects of an accelerating or de- 3. Physical shock model celerating synchrotron source in a curved,non-conicaland non- adiabatic jet. This model is confronted to the observations by In the original shock model of MG85, the shock front was as- fitting seventeen distinct outbursts simultaneously to thirteen sumed to propagate with constant speed in a straight conical submillimetre-to-radio light-curves of 3C 273. The proper pa- and adiabatic jet. Partial generalizations of this model were al- rameterization to achieve this fit is described in Sect. 4 and the ready derived by Marscher (1990) and Marscher et al. (1992) results of this light-curve decomposition are given in Sect. 5. in the case of a bending jet, and by Stevens et al. (1996) in In Sect. 6, we discuss the implications of our results, both on the two cases of a straight non-adiabatic jet and a curved adia- the global properties of the inner jet and on the peculiarities of batic jet. Here we further generalize the shock model of MG85 individual outbursts. The main results of this study are summa- to account for the effects of an accelerating or decelerating rized in Sect. 7. shock front in a curved, non-conical and non-adiabatic jet. In Sect. 3.1, we describe the typical three-stage evolution of all Throughout this paper, we use the convention +α for Sν ∝ν outbursts, whereas in Sect. 3.2 we show how the physical con- the spectral index and we use “ ”, rather than “ ”, for the α lg log ditions at the onset of the shock can influence the evolution of decimal logarithm “ ”, because of a lack of space in tables log10 individual outbursts. and long equations.
3.1. Typical three-stage evolution
2. Observational material Following MG85, we consider the synchrotron radiation emit- ted just behind a shock front in a cylindric portion of a jet hav- The light-curves fitted here are part of the multi-wavelength ing a radius R across the jet and a length x along the jet axis, database of 3C 273 presented by T¨urler et al. (1999a). The 12 as illustrated in Fig. 1. Within this volume, we assume that the light-curvesfrom 5GHz to 0.35mm are as described in Paper I, magnetic field B is uniform in strength and nearly random in except that we now consider the observations up to 1999, in- direction and that the relativistic electrons have a power law en- cluding the most recent measurements from the Mets¨ahovi Ra- ergy distribution of the form N(E)= K E−s, with N(E)dE dio Observatory in Finland and from the University of Michi- being the number density of the electrons. Measured in the rest gan Radio Astronomy Observatory (UMRAO). frame of the quasar, these synchrotron emitting electrons have We extend to lower frequencies the analysis of Paper I a relativistic bulk velocity β = v/c, with c being the speed of by adding a new light-curve at 2.7GHz. This light-curve is light, and a corresponding Lorentz factor Γ=(1 − β2)−1/2. constituted of observations from the Green Bank Interferom- As a consequence, the synchrotron emission observed with an eter (GBI) and from the 100m telescope at Effelsberg in Ger- angle θ to the jet axis is Doppler boosted with a bulk Doppler many (Reich et al. 1998). The fluxes obtained with the GBI factor given by D = Γ−1(1 − β cos θ)−1. We further assume at 2.7GHz and 2.25GHz include both 3C 273B (the inner jet) that the jet opening half-angle φ is smaller than θ at any time and 3C 273A (the hot spot at the far end of the jet), but these after the onset of the shock and that θ itself is small enough two components combine partially out of phase (Ghigo F.D., to verify sin (θ + φ) < 1/Γ, so that the line-of-sight depth of private communication). As a consequence, the GBI measure- the emitting region is directly proportional to its thickness x ments are only part of the total flux of 3C 273 and have to be (Marscher et al. 1992). multiplied by a scaling factor. The observed optically thin flux density Sν and turnover To scale the GBI measurements at 2.25GHz we use frequency νm of the self-absorbed synchrotron spectrum are the contemporaneous Effelsberg single dish observations at then given by 2.7GHz. The nearly flat spectral index of 3C 273 at this fre- quency (T¨urler et al. 1999a) allows us to neglect the small dif- 2 (s+1)/2 (s+3)/2 −(s−1)/2 Sν ∝ R xKB D ν and (1) ference in frequency.We obtain that the GBI fluxes at 2.25GHz 2/(s+4) (s+2)/2 (s+2)/2 have to be multiplied by 1.66 to fit the Effelsberg observa- νm ∝ xKB D , (2) tions. A similar calibration of the earlier GBI measurements at 2.7GHz is not possible due to the lack of contemporaneous 1 We obtain a best-fit value of 1.12 for this factor with the jet model single dish observations. We therefore let the scaling factor of presented in Sect. 5. M. T¨urler et al.: Modelling 20 years of synchrotron flaring in the jet of 3C 273 3
place of inner jet black hole shock onset x shock front
R 1/ r Fig. 1. Sketch of the jet geometry dis- θ L ~ R ✷ β c cussed in Sect. 3, as observed in the φ rest frame of the quasar. We assume the contribution of the inner jet to be neg- L = 0 ligible with respect to the synchrotron K on K ~ K R -k emission of the grey region behind the R = 0 region of synchrotron on Bon -b shock front. This cylindrical portion of emission B ~ Bon R D the jet is moving along the jet axis with on D ~ D -d on R a relativistic speed βc where K and B are measured in the comoving frame of the electrons. Due to the similarity between Compton and syn- emitting plasma and Sν , ν, νm, R, x and D are measured in the chrotron expressions of the cooling time tcool of the electrons, observer’s frame. the synchrotron limited thickness x2 of the emitting region is The thickness x of the emitting region behind the shock simply obtained by replacing uph in the expression of x1 by front is the crucial parameter that changes the outburst’s evo- uB, so that x2 becomes lution from one stage to the other. If radiative losses are the −3/2 1/2 −1/2 dominant cooling process of the electrons accelerated at the x2 ∝ B D ν . (4) shock front, x is approximatively given by 2 vrel tcool, where During the final stage of the shock evolution synchrotron losses vrel is the excess velocity of the shock front relative to the become less important than adiabatic expansion losses and the emitting plasma and is the typical cooling time of the tcool shock is assumed to remain self-similar so that x ∝ R. electrons.2 During the first stage of the shock evolution Comp- 3 By substituting x in Eqs (1) and (2) by the corresponding ton scattering is the dominant cooling process of the elec- expression of xi (i =1, 2, 3) for each of the three stages i of trons and the Compton limited thickness x1 of the emitting −1 1/2 1/2 −1/2 the shock evolution we obtain: region is given by x1 ∝ uph B D ν , where the en- (11−s)/8 (s+1)/8 (s+4)/2 −s/2 ergy density of the synchrotron photons uph can be expressed Sν,1 ∝ R B D ν (5) as u ∝ K (B3s+7 Rs+5)1/8 (Eq. (13) of MG85).3 By com- ph S ∝ R2 KB(s−2)/2 D(s+4)/2 ν−s/2 (6) bining these two equations, we obtain4 ν,2 S ∝ R3 KB(s+1)/2 D(s+3)/2 ν−(s−1)/2 (7) −(s+5)/8 −1 −3(s+1)/8 1/2 −1/2 ν,3 x1 ∝ R K B D ν . (3) −1/4 1/4 (s+3)/(s+5) νm,1 ∝ R B D (8) The shock evolution enters the synchrotron stage as soon 2 s−1 s+3 1/(s+5) νm,2 ∝ [ K B D ] (9) as the photon energy density uph is equal to the magnetic field 2 ν ∝ [ RKB(s+2)/2 D(s+2)/2 ]2/(s+4) . (10) energy density uB = B /(8π). During this second stage, syn- m,3 chrotron radiation is the dominant energy loss process of the Finally, by using these six last equations, it is straightforward 2 The centre of the emitting region is given by the typical distance to obtain the expressions for Sm,i ≡ Sν,i(νm,i) as vrel tcool from the shock front reached by the electrons in the upstream 11/8 1/8 (3s+10)/(s+5) direction before loosing substantially their energy. The full width x of Sm,1 ∝ R B D (11) the emitting region is thus about twice that distance. S ∝ R2 [ K5 B2s−5 D3s+10 ]1/(s+5) (12) 3 This calculation assumes that only first order Compton scattering m,2 2s+13 5 2s+3 3s+7 1/(s+4) is important. The effect of higher order Compton losses would be to Sm,3 ∝ [ R K B D ] . (13) steepen even more the initial rise of the spectrum (Marscher et al. 1992). We now assume that each of the quantities K, B and D 4 x1 and x2 in Eqs (3) and (4) are actually expressed in the comov- evolves as a power-law with the radius R of the jet and we ing frame of the emitting plasma. The transformation of xi to the ob- parameterize this evolution as server’s frame would be obtained by dividing these expressions by the −k −b −d Lorentz factor Γ to correct for length contraction and by multiplying K ∝ R B ∝ R D∝ R . (14) them by the Doppler factor D to correct for front-to-back time delay (Marscher A.P., private communication). This tricky transformation If we replace these relations into the expressions for νm,i is due to the non-spherical shape of the emitting slab, which appears and Sm,i (Eqs (8) to (13)), the turnover (νm,Sm) of the self- rotated in the observer’s frame (cf. Marscher 1987; Marscher et al. absorbed synchrotron spectrum will also evolve as a power-law 1992). However, since the viewing angle θ is assumed to be smaller with R during each stage i of the shock evolution as than about 1/Γ, D is proportional to Γ (e.g. Marscher 1980), so that ni fi fi/ni these two corrections cancel out when using proportionalities. νm,i ∝ R and Sm,i ∝ R ⇒ Sm,i ∝ νm,i , (15) 4 M. T¨urler et al.: Modelling 20 years of synchrotron flaring in the jet of 3C 273 where the exponents ni and fi are given by geometryof Fig. 1 and the basic principles of superluminalmo- tion (e.g. Pearson & Zensus 1987), we obtain n1 = −(b+1)/4 − d (s+3)/(s+5) (16) n2 = −[2k + b (s−1)+ d (s+3) ]/(s+5) (17) (1+z) sin θ (1+z) t = (L−Lon)= (L−Lon) , (23) βapp c βc Γ D n3 = −[ 2 (k−1)+(b + d)(s+2) ]/(s+4) (18) f1 = (11−b)/8 − d (3s+10)/(s+5) (19) where βapp is the apparent transverse velocity of the source in units of c and L measures the distance along the jet axis in f2 = 2 − [5 k + b (2s−5)+ d (3s+10) ]/(s+5) (20) the rest frame of the quasar. To continue working only with f3 = [2s+13 − 5 k − b (2s+3) − d (3s+7) ]/(s+4) . (21) proportionalities, we are forced to assume that Lon is small Marscher (1987) shows that even a geometrically thin with respect to L during the major part of the shock evolution, source in a relativistic jet appears inhomogeneous when ob- so that L−Lon tends rapidly towards L during, or just after, served with a small angle θ between the jet axis and the line- the Compton stage. Under this assumption and by considering 2 of-sight. The optical depth of the source will therefore depend that β Γ D is proportional to D for Γ ≫ 1 and θ ∼< 1/Γ (e.g. on the frequency, which has the effect of broadening the self- Marscher 1980), we have t ∝ D−2 L. Finally, by parameter- absorption turnover and leads to a lower optically thick spec- izing the opening radius R of the jet with the distance L as r −d tral index αthick than the typical value of +5/2, which holds R ∝ L and by remembering that D ∝ R (Eq. (14)), we for a homogeneous synchrotron source. To estimate the value obtain of the spectral index below the turnover frequency ν , we can m −2 1/r ρ with (24) cut the source into many self-similar cylindric portions of the t ∝ D R ∝ R ρ = (2rd + 1)/r . jet having a length l ≪ x proportional to their radius R and With this relation, the three-stage evolution of Eq. (15) can now chosen small enough for their synchrotron emission to be ho- be expressed as a function of time t rather than radius R, as mogeneous. The emitted spectrum of each section will have a βi with γ f self-absorption turnover (νm,Sm) depending on R according νm,i ∝ t βi ≡ ni/ρ i i γi ⇒ = , (25) to Eq. (15) with i =3, because in this case l ∝ R replaces x in Sm,i ∝ t with γi ≡ fi/ρ βi ni Eqs (1) and (2). The inhomogeneous source behind the shock where βi and γi are defined as in Paper I and depend now on front is therefore expected to have an optically thick spectral the five exponents s, r, k, b and d via the Eqs (16) to (21) for index of αthick = f3/n3 due to the superimposition of the ho- ni and fi (i=1, 2, 3). mogeneous spectra of the individual sections. However, the fi- nite size of the emitting region should limit the frequency range over which this flatter spectral index pertains. We therefore ex- 3.2. Specificity of individual outbursts pect a spectral break at a frequency νh (< νm), at which the We described in the previous section how the spectral turnover spectral index αthick =f3/n3 returns to its homogeneous value (νm,Sm) of the emitted synchrotron spectrum behaves accord- of +5/2. ing to the physical properties of the jet and during each of the A high-frequency spectral break is also expected in the op- three stages of the shock evolution. What we describe here is tically thin part of the spectrum due to a change in the elec- how the transitions from one stage to the other are influenced tron energy distribution induced by synchrotron and/or Comp- by the physical quantities at the onset of the shock. The first ton losses. In the case of continuous injection or re-acceleration transition from the Compton to the synchrotron stage is char- of electrons suffering radiative losses, the optically thin spectral acterized by the condition uph = uB, which corresponds to index αthin is expected to steepen by a value of −1/2 above a x1 = x2 and can be expressed by the proportionality frequency νb (Kardashev 1962). The break frequency νb of the spectrum in the observer’s frame is related to the break energy −(s+5) 8 3(s−3) R1|2 ∝ K1|2 B1|2 , (26) 2 Eb of the electron energy distribution as νb ∝ B D Eb (e.g. Marscher 1980). For our analysis at submillimetre-to-radio fre- where K1|2 ≡ K(t1|2), R1|2 ≡ R(t1|2) and B1|2 ≡ B(t1|2), quencies, the evolution of νb with the jet radius R is only rele- with the subscript 1|2 referring to the transition from the first vant during the final stage of the shock evolution. For adiabatic to the second stage of the shock evolution at a time t1|2 after expansion in two dimensions, the energy E of the electrons de- the onset of the shock. creases with R as E ∝ R−2/3 (e.g. Gear 1988). By using this A similar expression can be derived for the second transi- relation and Eq. (14), we find that the evolution of the break tion from the synchrotron to the adiabatic stage by imposing −3/2 1/2 −1/2 frequency νb during the adiabatic stage is given by that x2 = x3, which corresponds to R2|3 ∝ B2|3 D2|3 ν2|3 ,
b where , with the subscript referring to the ν ∝ Rn with n = −(4/3+b+d) . (22) ν2|3 ≡ νm(t2|3) 2|3 b,3 b transition from the second to the third stage of the shock evo- Until now, we related the spectral turnover (νm,Sm) and lution. By replacing ν2|3 in the condition above by the propor- the high-frequency spectral break nb to the radius R of the tionality of Eq. (9) for νm,2(t2|3) – or equivalently by that of emitting region. But since we are interested in the temporal Eq. (10) for νm,3(t2|3) – we obtain evolution of these quantities, we have to relate R to the ob- −(s+5) 2s+7 −1 served time t after the onset of the outburst. According to the R2|3 ∝ K2|3 B2|3 D2|3 . (27) M. T¨urler et al.: Modelling 20 years of synchrotron flaring in the jet of 3C 273 5
We can now further parameterize the proportionalities of Table 1. Expressions of the parameters U, V and W of Eqs (35) Eq. (14), as to (37) and of Eq. (40) for the logarithmic shifts ∆ lg P of the parameters P in the first column. These expressions character- −k −b −d K ∝ Kon R B ∝ Bon R D ∝ Don R , (28) ize the effect of varying the physical quantities K, B and D at the onset of the shock. where the subscript “on” refers to the onset of the shock. By including these relations expressed at the particular radii R = UVW R1|2 and R = R2|3 into Eq. (26) and Eq. (27), respectively, we 8ρ 3(s−3)ρ t1|2 −2 obtain ζ1|2 ζ1|2 ρ (2s+7)ρ ρ t2|3 −2− ζ2|3 ζ2|3 ζ2|3 ζ1|2 8 3(s−3) ζ2|3 2s+7 −1 R ∝ K B and R ∝ Kon B D , (29) 2 8n2 s−1 3(s−3)n2 s+3 1|2 on on 2|3 on on ν1|2 + + s+5 ζ1|2 s+5 ζ1|2 s+5 2 n2 s−1 (2s+7)n2 s+3 n2 ν2|3 + + − where the exponents ζ1|2 and ζ2|3 are given by s+5 ζ2|3 s+5 ζ2|3 s+5 ζ2|3 5 8f2 2s−5 3(s−3)f2 3s+10 S1|2 + + s+5 ζ1|2 s+5 ζ1|2 s+5 ζ1|2 ≡ 8k +3b(s−3) − (s+5) (30) S 5 + f2 2s−5 + (2s+7)f2 3s+10 − f2 2|3 s+5 ζ2 3 s+5 ζ2 3 s+5 ζ2 3 ζ2|3 ≡ k + b(2s+7) − d − (s+5) . (31) | | | nb (2s+7)nb nb νb,2|3 1+ 1 − ζ2|3 ζ2|3 ζ2|3 The expressions of Eq. (29) relate the radii R1|2 and R2|3 of the jet at which the two transitions 1|2 and 2|3 occur to the values of the physical quantities K, B and D at, or just after, for S, ν and t. The set of equations relating these shifts for the the onset of the shock. Any change of these quantities at the first transition can be written as onset of the shock will therefore have the effect of displacing 1/r the position in the jet (via L ∝ R ) at which the two tran- ∆lg t1|2 = Ut1|2 ∆lgKon +Vt1|2 ∆lgBon +Wt1|2 ∆lgDon (35) sitions occur. A stronger magnetic field B , for instance, will on ∆lg ν1|2 = Uν1|2 ∆lgKon +Vν1|2 ∆lgBon +Wν1|2 ∆lgDon (36) have the effect to prolong the synchrotron stage, by making it ∆lgS1|2 = US1 2 ∆lgKon +VS1 2 ∆lgBon +WS1 2 ∆lgDon. (37) start slightly further upstream in the jet and finish much further | | | downstream for a typical value of s ≈ 2 and comparable values Similar expressions can be written for the second transition by replacing 1|2 in Eqs (35) to (37) by 2|3. The 2 × 9 expressions of ζ1|2 and ζ2|3. of the parameters U, V and W obtained for both transitions are The values of Kon, Bon and Don, will also influence the displayed in Table 1. There is a great symmetry among these times t1|2 and t2|3 after the onset of the shock at which the parameters, which reflects the fact that the two equations two transitions are observed, as well as the frequencies ν1|2 and ν2|3 and flux densities S1|2 and S2|3 of the self-absorption ∆ lg ν2|3 − ∆ lg ν1|2 = β2(∆ lg t2|3 − ∆ lg t1|2) and (38) turnover (νm,Sm) at these times. By including the proportion- ∆ lg S − ∆ lg S = γ2(∆ lg t − ∆ lg t ) (39) alities of Eq. (28) into Eq. (24) for the observed time t and into 2|3 1|2 2|3 1|2 Eqs (9) and (12) for the evolution during the synchrotron stage must be verified, in accordance with Eq. (25). Finally, we can also derive the influence of , and of turnover frequency νm,2 and the corresponding flux density Kon Bon on the high-frequency spectral break , Sm,2, we obtain for the first transition Don νb,2|3 ≡ νb(t2|3) nb which is given by νb,2|3 ∝ Don Bon R2|3 (cf. Eq. (22)) and −2 ρ t1|2 ∝ Don R1|2 (32) corresponds to the logarithmic shift
1/(s+5) n2 s+3 2 s−1 ∆lg νb,2|3 =Uνb ∆lgKon +Vνb ∆lgBon +Wνb ∆lgDon, (40) ν1|2 ∝ Don Kon Bon R1|2 (33)