Standing and propagating waves in cubically nonlinear media
Full text
(2) PHYSICAL BACKGROUND The equation of motion of a continuous medium is [5] . ∂ 2Ui a t ρ0 ∂ t2. ∂ P Di j ∂aj ij . (1). where ρ0 is the density in the undeformed state, Ui is the displacement, Ui xi ai , of the particle originally at ai (Lagrangian coord.), Pi j is the stress tensor, Di j is the dissipative stress tensor. The elastic energy W is expanded in the invariants of the strain tensor E i j , Ei j . 1 ∂ Ui 2 ∂aj. ∂Uj . ∂ ai. . ∂ Uk ∂ Uk ∂ ai ∂ a j. (2). to the fourth order [6]:. ρ0 W . K 2 4. H Ekk . . µ C A 2 Ekk µ Ei j E ji Ekk 3 BEkk Ei j E ji E E E 3 3 3 i j jk ki G Ei j E ji 2 F Ekk 2 Ei j E ji EEkk Ei j E jl Eli DEi j E jk Ekl Eli. . Using the relation Pi j . ρ0. ∂W. (4). ∂ Ui ∂aj . ∂. we obtain from (1) and (3) the equations of motion, with the notation Ui j. ρ0 . ∂ Di ∂t . . ∂ 2Ui ∂ t2 . ct2. (3). ∂ 2Ui ∂ a2k. . c2l ct2 . . ∂ Ui , ∂aj. ∂ Ukk
(3) ∂ ai. ∂ K µ UklUkl δis 2UkkUis UklUklUis . ∂ as 2 3
(4) µ UikUsk UikUks UkiUks UikUrkUrs . . (5). where "..." stands for terms of second and third order in Uik with coefficients A, B, C, D, E, F , G, H, and ct and cl are the transverse and longitudinal wave propagation velocities respectively, K 43µ µ 2 2 c ct (6) ρ0 l ρ0. The dissipative term. ∂ Di ∂t. Di . in (5) is obtained from. η. ∂ 2Ui ∂ a2k . ∂ 2Uk ∂ ai ∂ ak . ζ . ∂ 2Uk 2 η 3 ∂ ai ∂ ak. (7).
(5) where η , ζ are the shear and bulk viscosities respectively. With the scalings a1 U1 . 1 2. ε. 1. . U1 . ε 2 a1 a2 U2. ε . η. . 1. ε 2 a2 1 2. U2 . ε . 1. U3. η. ε a3. a3 . . ε. ζ . 1. ε. U3 1. ζ. (8). a nonlinear beam equation can be derived [6] for transverse waves, vibrating in the 1-direction and propagating in the 3-direction. In this case the quadratic nonlinearity ∂U cancels and the equation for ∂ t 1 V becomes. ∂ ∂V ∂τ ∂z . β 2 ∂V V ct3 ∂ τ. δ . a3 c3 . where x y z τ is given as a 1 a2 a3 t . δ. β . 3 K. 2 2ρ0 ct 2 . 2µ 3 . B. ∂ 2V
(6) ∂ τ2 . . ∂2
(7) V ∂ y2. (9). and δ and β are given as. η 2ρ0 ct3 . A D G 2 2. ct ∂ 2 2 ∂ x2. . K 2 . (10). 2µ 3 . 3B 4 . A 4. K. K µ 3. 4µ 3 . B. A 2
(8). (11). The quotient term in (11), because of which β can be negative, is missing in the paper by Zabolotskaya [6]. The equation (9) is studied by Rudenko and Sapoznikov [9]. If K and µ are the only elastic constants different from zero in (11) we obtain using (6):. β . . 3 c2l 4 c2l ct2. (12). Thus β is negative for the simplest solid materials.. STANDING WAVES IN A CUBICALLY NONLINEAR RESONATOR Neglecting dissipation and transverse extension Eq. (9) becomes. ∂V ∂z . β 2 ∂V V c3 ∂ τ . 0. (13). where ct is replaced by c in order that Eq. (13) be applied to other physical phenomena than transverse waves in solids. The choice of the negative sign in the definition of τ means that Eq. (13) describes rightgoing waves. Standing waves in a resonator are.
(9) composed by waves propagating in both directions. A wave equation, which gives Eq. (13) when specialized to rightgoing waves, is (change z into x):. ∂ 2V ∂ x2 . 1 ∂ 2V c2 ∂ t 2. . 2β ∂ 2V 3 3c4 ∂ t 2. (14). The equation with a quadratic nonlinearity corresponding to the cubic nonlinear equation (14) is studied for a resonator by the present authors [7]. The resonator boundary conditions are V x 0 t A sin ω t V x L t 0. (15) In analogy with the solution attempted by the present authors for a quadratic nonlinearity [7] we attempt a solution to Eq. (14) in the form V . V . . V. V . . . ω x L c . F ωt . βω I F 2 x L c3 2 I V . (16). Inserting (16) into the boundary conditions (15) gives a functional equation F ω t kL . βω I F 2 x L c3 . F ω t kL . βω I F 2 x L c3 ω A sin ω t k c. (17). The functional equation (17) can be reduced to a differential equation with dimensionless variables:. ∂W ∂t . ∆ πβ J πβ W 2 . ∂W ∂ξ. D . with. F A ωt π T M ξ c c The discrepancy ∆ in Eq. (18) is defined as W. . ∆ . ω ω0 ω0. . ∂ 2W ∂ξ2 . ωt π. . M sin ξ 2. J . I c2. (18). (19). (20). with ω πcL (lowest resonance frequency of the resonator). The dissipation coefficient D in Eq. (18) is defined as D. bω L 2c3 ρ0. . 1. (21). where the absorption coefficient b ( η and ζ ) can be introduced in Eq. (18) in analogy with its occurrence in Burgers’ equation [1]..
(10) FIGURE 1. Quadratic resonator root-mean-square velocity as function of discrepancy parameter ∆ πε . The curves are for different boundary vibration amplitudes.. FIGURE 2. The cubic resonator frequency response as a function of discrepancy parameter δ . The curves are (from above) for different absorptions: d=0.4, 0.5, 0.75, 1.25, 2.. Frequency response functions for a quadratic and a cubic nonlinear resonator are plotted in Fig. 1 and Fig. 2 respectively. In Fig. 1 we plot the rms normalized particle ∆ velocity W 2 as function of the normalized discrepancy πε , where ε is the quadratic nonlinearity parameter. Curves 1-5 are constructed for different values of boundary M 2 vibration [ πε 10 = 1, 4, 9, 16 and 25]. In Fig. 2 a frequency response function y δ with 1 I 3 2πβ 2 16 y 2 3 δ ∆ 3 (22) 2 c M 3πβ M is constructed for different values of the normalized absorption coefficient 1 [d D 3 M2πβ 3 = 2, 1.25, 0.75, 0.5 and 0.4]..
(11) W θ. 1. 1. θ. −1. −1. 1 θ −1. X=X2 > X1. X = X1. X=0 FIGURE 3.. W. W. Schematic evolution of an original N-wave in a cubically nonlinear medium.. PROPAGATING N-WAVES IN A CUBICALLY NONLINEAR MEDIUM The modified Burgers’ equation for plane waves. ∂V ∂z . β 2 ∂V V ct3 ∂ τ. δ . ∂ 2V ∂ τ2. (23). following from (9), has to be made dimensionless. To this end we introduce a fundamental period ν t0 1 , where t0 is the duration of the N-wave at the boundary, and the velocity amplitude V0 at the boundary. The dimensionless equation derived from (23) is. ∂W ∂X with W. . . V V0. X. . . . W2. ∂W ∂θ. 2 β V02 ν z ct3. ε . θ . ∂ 2W ∂θ2 2ντ ε. (24). . ην β ρ0V02. (25). We assume β 0 and ε 1. The equation (24) has been studied by Lee-Bapty and Crighton [10]. The qualitative deformation of an original N-wave for increasing X -values according to Eq. (24) with ε 0 is shown in Fig. 3. The multivalued parts of the profile in the last picture of Fig. 3 are replaced [10] by a 1 1 tail shock at θ Ct X 1 d 2X 4 and a head shock at θ Ch X 1 3d 2X 4 with d 0 95. The structures of the shocks and of the tail at θ 1 are found by rescaling Eq. (24), so that the righthand side is no longer small. By this procedure seven parts of the profile are discerned, satifying different scaled versions of Eq. (24) with different dominant terms (Fig. 4). The new results in the present paper concern part 1 (left tail) and part 2 (connection at θ 1 between left tail and left curve). For parts 3 (left curve), 4 (tail shock), 5 (right curve) and 6 (head shock) analytic lowest approximation solutions are given by Lee-Bapty and Crighton [10]. For part 7 (right tail) an analytic solution is still not yet found. . . . .
(12) (3) (4) (2) (1) -1. -1. (7). (6). (5). FIGURE 4.. The seven parts of the deformed N-wave in a cubically nonlinear medium.. We first attempt to find a solution for part 2, because this solution has to be consistent with the part 1 and part 3 solutions. The scalings X. 1. ε2X . θ. θ . . ε. 1 1 2. . 1. W. ε 2W . 1. W0 . . O ε2. (26). are inserted into (24) and give in lowest order W0 2. ∂ W0 ∂θ . ∂ 2W0 ∂θ 2. (27). The solution of (27) with the necessary consistency properties is W0 . ε. 1 2. W0. 3 2 . 1. ε4 . . C ε2 θ 1. (28). 1 . where the constant C can be determined numerically. The solution (28) is valid for. θ 1. . 1. 1. 2ε 2 X 2 . θ. . 1. (29). . 3 1X ε 2 θ 1. (30) 2 C The independence of the solution (28) on X is seen in the numerically calculated solution in Fig. 5, where all profiles for different X have approximately the same value for θ 1. For part 1 (left tail) we make the scalings. θ. ξ. 3. . ε2X. ζ. . 1. . 1. . . ε4 θ . 1 . U . ε. 7 8. W. 1. . U0 O ε 2 . (31).
(13) 1. z= 0, 0.5, 0.7, 0.9, 1.1, 1.3. 0.8 0.6 0.4 0.2 0 - 0.2 - 0.4 - 0.6 - 0.8 -1 -2. - 1.5. -1. - 0.5. 0. 0.5. 1. 1.5. 2. 0 005 for X. FIGURE 5. Numerical solutions of Eq. (24), evaluated with ε. 0 0 5 0 7 0 9 1 1 1 3 .. which are inserted into (24) and give a lowest order linear equation. ∂ U0 ∂ξ. ∂ 2U0 ∂ζ2. . (32). The equation (32) is identically solved by the integral representation. . U0. ∞. K . 0. h λ exp iλ ζ K. 3 ε 8π . λ 2ξ d λ 1 2. . h λ . c c. . 1 2. λ. . (33). where c.c. stands for complex conjugated and K and h λ are chosen so that the solution (33) matches the solution (28). This is seen by evaluating the integral in (33) by the steepest descent method with X and θ inserted from (31) with the result W0. 3 θ 2. 7. . ε 8 U0 . 1 . 1 2. exp . θ 1 4ε X. 2. . (34). Solutions (28) and (34) match each other in the region where (29) is fulfilled together with 1 θ 1 Cε 2. (35) . For part 3 (left curve) the expansion W. ∂ W0 ∂X . W02. ∂ W0 ∂θ. . . W0 O ε gives using (24) [10]. 0. . θ. W0 . 1 . X. (36). 1. (37). For the solution (36) to be valid we must require (cf. Eq. 24). ε. ∂ 2W0 ∂θ2. . ∂ W0 ∂X. . θ. 1 εX . 2 . .
(14) Thus for X O 1 the transition from the solution (37) to the solution (28) is completed 1 at θ 1 O ε 2 . A representation similar to (34) for the right tail remains to be found, ε 2 (cf. the scaling as well as an exponentially decreasing profile at both ends for X (31)). . . REFERENCES 1. O.V. Rudenko, and S.I. Soluyan, Theoretical Foundations of Nonlinear Acoustics, Plenum, Consultants Bureau, New York, 1977. 2. P.L. Sachdev, Nonlinear Diffusive Waves, Cambridge University Press, Cambridge, 1987. 3. B.O. Enflo, and C.M. Hedberg, Theory of Nonlinear Acoustics in Fluids, Kluwer, Dordrecht, 2002. 4. D.G. Crighton, and J.F. Scott, Asymptotic solutions of model equations in nonlinear acoustics. Phil. Trans. R. Soc. Lond. A 292, 101–134 (1979). 5. A.N. Norris, “Finite amplitude waves in solids”, in Nonlinear Acoustics, edited by M.F. Hamilton, and D.T. Blackstock, Academic Press, San Diego, 1998, pp. 263–277. 6. E.A. Zabolotskaya, Sound beams in a nonlinear isotropic solid, Sov. Phys. Acoust. 32, 296–299 (1986). 7. B.O. Enflo, C.M. Hedberg, and O.V. Rudenko, Resonant properties of a nonlinear dissipative layer excited by a vibrating boundary: Q-factor and frequency response, J. Acoust. Soc. Am. 117, 601–612 (2005). 8. B.O. Enflo, On the connection between the asymptotic waveform and the fading tail of an initial N-wave in nonlinear acoustics, Acustica - Acta Acustica 84, 401–413 (1998). 9. O.V. Rudenko, and O.A. Sapoznikov, Wave beams in cubically nonlinear nondispersive media, JETP 79, 395–413 (1994). 10. I.P. Lee-Bapty, and D.G. Crighton, Nonlinear wave motion governed by the modified Burgers equation. Phil. Trans. R. Soc. Lond. A 323, 173–209 (1987)..
(15)
Related documents
DIN representerar Tyskland i ISO och CEN, och har en permanent plats i ISO:s råd. Det ger dem en bra position för att påverka strategiska frågor inom den internationella
The government formally announced on April 28 that it will seek a 15 percent across-the- board reduction in summer power consumption, a step back from its initial plan to seek a
18 http://www.cadth.ca/en/cadth.. efficiency of health technologies and conducts efficacy/technology assessments of new health products. CADTH responds to requests from
Energy issues are increasingly at the centre of the Brazilian policy agenda. Blessed with abundant energy resources of all sorts, the country is currently in a
Det finns många initiativ och aktiviteter för att främja och stärka internationellt samarbete bland forskare och studenter, de flesta på initiativ av och med budget från departementet
Den här utvecklingen, att både Kina och Indien satsar för att öka antalet kliniska pröv- ningar kan potentiellt sett bidra till att minska antalet kliniska prövningar i Sverige.. Men
Av 2012 års danska handlingsplan för Indien framgår att det finns en ambition att även ingå ett samförståndsavtal avseende högre utbildning vilket skulle främja utbildnings-,
Det är detta som Tyskland så effektivt lyckats med genom högnivåmöten där samarbeten inom forskning och innovation leder till förbättrade möjligheter för tyska företag i