rsos.ro yalsocietypublishing .org Resear ch Cite this ar ticle: P opov VL, L yashenk o IA, Filippo v AE. 2017 Influence of tangential displacement on the adhesion str ength of a contact between a parabolic pr ofile and an elastic half-space. R. Soc . open sci. 4 : 161010. http://dx.doi.or g/10.1098/rsos.161010 Receiv ed: 7 December 2016 Acc epted: 1 August 2017 Subjec t Categor y : Physics Subjec t Areas: applied mathema tics/mathematical modelling/mechanics Key words: adhesion, friction, tribology , shear forc e, numerical simulation, method of dimensionality reduction Author for correspondence: V alen tin L. P opov e- ma i l: v [email protected] Influenc e of tangential displac ement on the adhesion str ength of a c ontac t bet w een a par abolic pr ofile and an elastic half-space V alentin L. P opov 1,2,3 , Iak ov A. L yashenk o 1,4 and Alexander E. F ilippov 1,5 1 Institut für Mechanik, FG Systemdynamik und Reibungsphysik, T echnische Univ ersität Berlin, Sekr . C8-4, Raum M 122, Straße des 17. Juni 135, 10623 Berlin, Germany 2 National Resear ch T omsk State Univ ersity , 634050 T omsk, Russia 3 National Resear ch T omsk Polyt echnic University , 634050 T omsk, Russia 4 Depar tment of Applied Mathematics and C omplex S ystems Modelling , F aculty of Electronics and Informational T echnologies , Sumy Stat e University , 40007 Sumy , Ukraine 5 National A cademy of Science, Donetsk Institute for Physics and Engineering , 83114 Donetsk, Ukraine VLP , 0000-0003-0506-3804 ;I A L , 0000-0001-7511-3163 The adhesion stre ngth of a contact between a rotationally symmetric indenter and an elastic half-space is analysed analytically and numerically using an extension of the method of dimensionality reduction for superimposed normal/tangential adhesive contacts. In particular , the dependence of the critical adhesion force on the simultaneously applied tangential for ce is obtained and the relevant dimensionless parameters of the pr oblem are identified. The fracture criterion used coincides with that suggested by Johnson. In this paper , it is used to develop a method that is applicable straightforwardly to adhesive contacts of arbitrary bodies of r evolution with compact contact area. 1. Intr oduc tion Johnson, Kendall and Roberts developed in 1971 their classical theory of normal adhesive contact between two parabolic, isotropic elastic bodies (JKR theory) [ 1 ] using the similarity between the boundary of an adhesive contact and the tip of a 2017 The Authors . Published by the Ro yal Society under the terms of the Cr eative C ommons Attribution License h ttp://creativ ecommons.or g/licenses/by/4.0/, which permits unr estric ted use, pr ovided the original author and sourc e are cr edited. 2 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ mode I crack (opening mode). They applied the same idea of the energy balance that Grif fith used in his classical theory of cracks [ 2 ]. In the subsequent years, the theory of adhesive contacts developed rapidly [ 3 ], mostly using various concepts developed in fracture mechanics. In the JKR theory—just as in the theory of Griffith—the equilibrium configuration of an adhesive contact is determined by minimizing the total energy of the system including the ener gy of elastic deformation of contacting bodies, the interface energy and the work of external for ces [ 4 ]. As this energy does not depend on the tangential displacement, the adhesive contact formally has no ‘tangential strength’. This appar ently contradicts experimental observations. The contradiction is due to the microscopically heter ogeneous structur e of any interface (at the atomic scale, if not earlier), which provides finite contact str ength in the tangential dir ection. From the micr oscopic point of view , one can interpret the fractur e criterion of Grif fith as the requir ement that the str ess at a fixed distance (of atomic order) fr om the actual ‘crack tip’ reaches some critical value (stress criterion). This condition leads to the macr oscopic dependence of the critical stress on crack length, which is identical to r elations obtained fr om the macroscopic ener gy balance [ 5 ]. Alternatively , one could r equir e that the relative displacement of the faces of the crack achieve some critical value (deformation criterion). The stress and deformation criteria ar e equivalent for purely elastic bodies, but can lead to differ ent fracture conditions in elastomers [ 5 ]. In this paper , we will only deal with purely elastic bodies, so we can apply either the str ess or the deformation criterion without loss of generality . Johnson studied the pr oblem of adhesive contact under superimposed normal and tangential loading [ 6 ] and concluded that, ‘when tangential for ces are applied to an adhesive contact the consequences are not at all well understood’. This situation has not changed much until now . In his paper of 1997, Johnson approaches the problem of adhesive contact under superimposed normal and tangential loading by considering the complete energy r elease rate at the boundary of an adhesive contact [ 6 ] Q = 1 2 E ∗ K 2 I + K 2 II + 1 1 − ν K 2 III , (1.1) where K I , K II and K III ar e the str ess concentration factors defined as K I,II,III = F I,II,III 2 a √ π a , (1.2) with a being the contact radius and F I , II , III the components of the applied force in the normal (I) and tangential directions (II, radial dir ection; III, tangential to the boundary line). The problem of a cir cular contact remains axially symmetric only if the Poisson number is zer o, ν = 0. In this case, the stress concentration factors for the modes II and III are e qual along the entire boundary line. In the case of arbitrary Poisson number , Johnson suggests to evaluate the average values of K II and K III ar ound the periphery of the contact area, simplifying (1.1) to Q = 1 2 E ∗ K 2 I + 2 − ν 2 − 2 ν K 2 II . (1.3) In terms of energy r elease rates, the condition of fracture can be formulated by equating the ener gy release rate to some critical value r elated to the work of adhesion γ . W e would like to stress that this approach is by no means self-evident. Physically , it means that elastic energy components due to normal and tangential loading contribute in equal manner to the destruction of interfacial bonds. This may be true in some cases. For example, if some polymer molecules that have to be br oken by sufficiently lar ge elongation mediate the adhesion of surfaces, then both normal and tangential deformations have to be considered when applying the ‘fractur e criterion’. The same may be valid in a contact of atomically smooth surfaces with equal characteristic range of atomic interaction in normal and tangential dir ections. In this case, the tangential displacement of atoms at the interface will bring them into a higher ener getic position compared with ‘unstr essed’ atoms. Subsequently , a smaller amount of work will have to be performed by normal for ces to complete the detachment. In this case, too, one can at least qualitatively assume that both normal and tangential parts of elastic energy give appr oximately the same contribution to the overall detachment energy . In other situations, however , this criterion can fail completely . Thus, if the characteristic range of atomic interactions in the in-plane dir ection is much smaller than in the normal direction, then the work of adhesion will be practically independent of the tangential loading and the criterion (1.3) will not be valid. One can also imagine a physical model, in which there is some ‘microscopic friction’ between surfaces that ar e pr essed to each other by relatively long-range van der W aals forces. In this case, the work of detachment will depend on the exact ‘dir ection of detachment’, as was suggested in [ 7 ]. Thus, the correct condition for the equilibrium of an adhesive contact under 3 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ tangential loading cannot be determined from pur ely theor etical considerations, as it may depend on the specific physics of the interface. Another important question in considering adhesion is what happens after the detachment takes place at some position on the boundary of adhesive contact. If the detachment occurs due to combined action of normal and tangential loading, then it may well be the case that the adhesion bonds will be restor ed after the medium has r elaxed the tangential part of elastic energy . This rebinding can actually take place, if it is not prevented by other factors. The simplest such factor may be a rapid change of the surface (e.g. due to oxidation). Another reason may be irr eversible changes of surface topography during detachment (so that the surfaces become incongruent and cannot r estore the initial configuration). Finally , the actual work of d etachment may be much lar ger than the pure surface ener gy . In this case, the main part of elastic energy will disappear irr eversibly and the relatively weak interfacial interactions will not be able to restor e the integrity of the interface again. In all these cases, we would have an irreversible adhesive contact . In this paper , we consider exactly this case of irr eversible adhesion. One can interpret this case as a fracture pr oblem of initially glued contact. In the following, we do not consider the physics of the interface in detail, but just make assumptions similar to those of Johnson, and use the method of dimensionality r eduction (MDR) for analysis of critical detachment conditions in analogy to the MDR formulation for the normal adhesive contact [ 8 ]. In a series of papers, Popov and co-authors have shown that contact pr oblems of axially symmetric three-dimensional bodies (under the additional assumption of compact contact area) can be equivalently repr esented by contacts with one-dimensional series of independent springs [ 5 ]. It is important to note that the results for axially symmetric contacts obtained with MDR ar e exact , and not an appr oximation, as is often believed. The MDR was first proposed 2007 for non-adhesive contacts [ 9 ], in which case it simply coincides with the solution of Galin & Sneddon [ 10 , 11 ]. In his dissertation of 2011, Heß derived the MDR formulation for adhesive contacts of arbitrary axis-symmetric bodies [ 12 ]. A short re view of the MDR for contacts of bodies of revolution can be found in [ 8 ]. Let us briefly mention previous appr oaches to the pr oblem of adhesion under superimposed normal and tangential load. In [ 13 ], the authors used the discrete element method for modelling contacts between cohesive, frictional particles with normal and tangential loading taking into account adhesion forces between the particles. In [ 14 ], a model of tangential adhesion contact was pr oposed, which, however , r equires the assumption that the ef fects of normal and tangential for ce can be considered independently . In this investigation, the authors showed that in the tangential contact problem the influence of adhesion can be appr oximately described in terms of equivalent load. In a series of articles by Guduru and co-authors [ 15 – 18 ] the work of adhesion was consider ed as a function of ‘mode- mixing’, which means that the work of adhesion depends on the dir ection of detachment [ 7 , 19 ]. In [ 15 ], the theory of Guduru et al. was verified experimentally . T angential adhesion effects wer e investigated numerically within the framework of coupled Eulerian–Lagrangian method in [ 20 ]. In [ 21 ], adhesion- induced plastic deformation due to tangential loading was considered. T angential adhesion ef fects have been investigated in the context of biological systems [ 22 , 23 ] and physics of particle interactions [ 13 , 24 , 25 ]. This paper is organized as follows. In §2, we r ecapitulate briefly the MDR appr oach for normal adhesive contacts and extend it for the case of superimposed normal and tangential loading under load-controlled and displacement-contr olled conditions. The model is then studied numerically and analytically and the dependence of the adhesive for ce on the tangential force is established in pr oper dimensionless variables. In §3, we describe the numerical procedur e in detail and compar e the numerical and analytical results. Section 4 concludes the paper . 2. Method of dimensionalit y r educ tion formulation f or adhesive c ontact and analytical solution 2.1. Method of dimensionality reduction for normal adhesive con tac ts W e start our consideration with a short introduction to the MDR. Let us consider a contact between an elastic continuum and a rigid, axially symmetric indenter having the shape f ( r ), where r is the polar radius in the contact plane. If the penetration depth d is known as a function of the radius a of the contact: d = g ( a ), (2.1) 4 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ d a D l max ( a ) g ( x ) 0 x z F z F x f ( r ) r 0 r z F z F x ( a )( b ) Figu re 1. MDR transformation of ( a ) the original thr ee - dimensional profile f ( r )i n t o( b ) a one - dimensional image g ( x ) and replac ement of the elastic half-space by an elastic founda tion. In the presenc e of normal and tangential for ce and adhesion, the springs of the elastic foundation will be displaced both in the normal and tangential dir ec tions. In this figur e, only v er tical displacements ar e shown. then the normal force F N can be r epr esented as a function of penetration depth by the trivial equation F N = F N 0 d ˜ F N = a 0 d ˜ F N d ˜ d d ˜ d d ˜ a d ˜ a = a 0 k ( ˜ a ) d g ( ˜ a ) d ˜ a d ˜ a = a 0 d k ( ˜ a ) d ˜ a ( d − g ( ˜ a ))d ˜ a , ⎫ ⎪ ⎪ ⎪ ⎬ ⎪ ⎪ ⎪ ⎭ (2.2) where k ( ã ) is the stif fness of a cylindrical punch with radius ã . Equations (2.1) and (2.2) can be interpr eted as the result of the indentation of a modified pr ofile g ( ã ) into an elastic foundation with independent springs with spacing d ã and stiffness (1/2)(d k ( ˜ a )/d ˜ a )d ˜ a . This interpretation is the basis of the MDR for both homogeneous [ 8 ] and non-homogeneous media [ 26 ]. In accordance with equations (2.1) and (2.2), the use of MDR is possible under two conditions: (i) the contact stif fness k ( ã ) of a cylindrical stamp with ar a d i u s ã must be known and (ii) the rule of determining the modified pr ofile g ( ã ) is known. Depending on the circumstances, these two steps may be performed analytically , numerically or experimentally . For homogeneous media, the rule for finding the modified pr ofile g ( ã ) is known explicitly . In the following, we will denote the ar gument of this function by x as is usually done in the MDR. However , in this context x does not denote any spacial coordinate but the internal variable of the MDR. The initial three-dimensional pr ofile f ( r ) (shown in figur e 1 a ) is first replaced by the one-dimensional pr ofile g ( x )b y means of the transformation [ 8 ]: g ( x ) =| x | | x | 0 f ( r ) x 2 − r 2 d r . (2.3) If needed, the original surface z = f ( r ) can be always restor ed fr om its MDR-transformed one-dimensional profile by f ( r ) = 2 π r 0 g ( x ) r 2 − x 2 d x . (2.4) In this paper , we will limit ourselves to parabolic pr ofiles of the form f ( r ) = r 2 /(2 R ). However , generalization to arbitrary rotationally symmetric profiles is straightforward. In the case of the parabolic profile, transformation (2.3) leads again to a parabolic pr ofile g ( x ) with a changed coefficient: f ( r ) = r 2 2 R ⇒ g ( x ) = x 2 R . (2.5) In the second step [ 8 ], the elastic half-space must be replaced by an elastic foundation, as shown in figure 1 , consisting of independent springs having normal and tangential stiffness k z = E ∗ x and k x = G ∗ x , (2.6) where x is the spacing of the springs and the ef fective moduli E *a n d G * are defined as E ∗ = E 1 − ν 2 = 2 G 1 − ν , G ∗ = 4 G 2 − ν , (2.7) 5 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ so that G ∗ = E ∗ 2 − 2 ν 2 − ν . (2.8) Note that in the case of ν = 0 both effective moduli coincide: E * = G *. For definiteness and simplicity , all numerical simulations and analytical calculations below are performed under this assumption. Before pr oceeding to tangential contacts, we will first r ecapitulate the application of the MDR to normal adhesive contacts. If the MDR-transformed profile g ( x ) is indented into the elastic foundation by an indentation depth d , then the displacement of individual springs inside the contact will be determined by the equation u z ( x ) = d − g ( x ) = d − x 2 R . (2.9) The size of the adhesive contact at a given indentation depth can be easily found from the principle of virtual work: the springs at the boundary of contact are str etched by l =− u z ( a ). The ener gy released through detachment of two boundary springs is equal to E ∗ l 2 x . Through detachment, the fr ee surface energy 2 π a x γ is cr eated (this ener gy can only be defined in the original, three-dimensional system). According to the principle of virtual work, the system will be in equilibrium if these two energies are equal: E ∗ l 2 x = 2 π a x γ . (2.10) It follows that the condition of equilibrium of boundary springs can be written as l = l max ( a ) = 2 π a γ E ∗ . (2.11) This condition is known as the rule of Heß [ 12 ]. Combining (2.9) and (2.11), we get u z ( a ) = d − a 2 R =− l max ( a ) =− 2 π a γ E ∗ (2.12) or d = a 2 R − 2 π a γ E ∗ . (2.13) The normal for ce can be calculated as the sum of all spring forces: F z ( a ) = E ∗ a − a u z ( x )d x = 2 E ∗ a 0 d − x 2 R d x = 4 E ∗ a 3 3 R − 8 π a 3 E ∗ γ . (2.14) Later we will consider a more general situation, wher e the indenter is also displaced in the tangential direction by u (0) x . It is convenient to present both analytical and numerical r esults in terms of dimensionless variables: ˜ a = a a 0 , ˜ F z = F z F 0 , ˜ d = d d 0 , ˜ u (0) x = u (0) x d 0 , ˜ u z = u z d 0 , (2.15) where F 0 , a 0 and d 0 ar e the critical values of the for ce, the contact radius and the absolute indentation depth at the moment of detachment of the parabolic profile fr om the elastic half-space under for ce- controlled conditions [ 4 ]: F 0 = 3 2 π R γ , a 0 = 9 π R 2 γ 8 E ∗ 1 / 3 , d 0 = 3 π 2 R γ 2 64 E ∗ 2 1 / 3 . (2.16) In dimensionless variables, equations (2.13) and (2.14) take the form ˜ d = 3 ˜ a 2 − 4 ˜ a 1 / 2 (2.17) and ˜ F = ˜ a 3 − 2 ˜ a 3 / 2 . (2.18) These results of course coincide with the classical solution of Johnson et al. [ 1 ]. The dependence of the dimensionless normal force on the dimensionless appr oach (indentation depth) implicitly defined by equations (2.17) and (2.18) is shown in figure 2 and will be used for testing numerical pr ocedures described in §3. W e now analyse the condition of instability of the contact, i.e. the conditions under which the possibility of the adhesive contact to sustain equilibrium is lost. W e will consider both displacement- controlled and load-contr olled contacts. Under displacement-controlled conditions, the macr oscopic 6 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ –2 0 2 4 6 –1 0 1 2 d ~ d ~ F ~ z F ~ z –2 0 2 4 6 –1 0 1 2 ( a )( b ) Figu re 2. Dependence of the normal for ce on the indentation depth for the normal contact with adhesion. Solid lines show the analytical solution defined by equations (2.17) and (2.18). Cir cles r epresent r esults of numerical experiments for displac ement- contr olled ( a )a n d load- contr olled ( b ) conditions as described in §3. displacement of the indenter is imposed by a very stiff external system. Physically , this means that during the movement of the system towards the equilibrium state, the displacement is kept exactly constant. Load-controlled c onditions are physically r ealized by applying the given force thr ough a very soft spring. Thus, in conditions of load control, the force during the r elaxation to the equilibrium r emains fixed. The method described in this section has been used successfully for modelling the influence of adhesion on impact between elastic particles under displacement-controlled conditions [ 25 ]. 2.2. Superimposed normal and tangential loading Let us now assume that the loading of the profile consists of superimposed normal for ce and tangential displacement u (0) x . The energy r eleased by detachment of two boundary springs will now be equal to E ∗ u z ( a ) 2 x + G ∗ u (0)2 x x . Equating this to the work of adhesion 2 π a x γ , we arrive at the following equilibrium condition: E ∗ u z ( a ) 2 + G ∗ u (0)2 x = 2 π a γ . (2.19) This rule is exactly equivalent to the rule obtained by Johnson on the basis of the ener gy r elease rate (1.3). From (2.19), for the elongation of the boundary springs we get | u z ( a ) |= 2 π a γ E ∗ − G ∗ E ∗ u (0)2 x . (2.20) Using (2.9), we can write the relationship between the indentation depth and contact radius in the form d = a 2 R − 2 π a γ E ∗ − G ∗ E ∗ u (0)2 x . (2.21) The normal and tangential forces ar e functions of contact radius a : F z = 2 E ∗ ad − a 3 3 R (2.22) and F x = 2 G ∗ a · u (0) x . (2.23) In dimensionless variables (2.15), equations (2.21)–(2.23) can be written as ˜ d = 3 ˜ a 2 − 16 ˜ a − G ∗ E ∗ ˜ u (0)2 x , (2.24) ˜ F z = ˜ a 2 ( ˜ d − ˜ a 2 ) (2.25) and ˜ F x = G ∗ 2 E ∗ ˜ a · ˜ u (0) x . (2.26) These equations determine the normal for ce–indentation relation in the pr esence of tangential displacement. Note that substitution of (2.24) into (2.25) at ˜ u (0) x = 0 reduces to the result (2.18) for the normal contact. 7 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ F ~ z D F ~ z F ~ x F ~ x 01 2345 –1 0 1 2 3 4 5 0 0.5 1 1.5 2 2.5 –0.5 0 0.5 02 46 81 0 0.1 0.2 0.3 0.4 0.5 ( a )( b ) Figu re 3. ( a ) The dependence of normaliz ed critical normal forc e ˜ F z on normalized critical tangen tial force ˜ F x , for the case E * = G *. Analytical results ar e repr esented b y solid lines and the results of numerical simulation b y open circles , diamonds, stars and triangles . The upper line ( diamonds and stars) corresponds to displacemen t control in both dir ections. The lo wer line ( open circles and triangles) corr esponds to load contr ol in the vertical direction and displacement contr ol in the tangential dir ec tion. Diamonds and open circles (r ed lines) corr espond to detachment at a negative indenta tion depth d . Stars and triangles correspond to detachment at a positive indentation depth; ( b ) the differenc e between the normal forc es shown in ( a ) as a function of normalized tangential for ce ˜ F x . Let us str ess that equation (2.19) assumes that the work of adhesion does not depend on the direction in which the surfaces are detached fr om each other . This is a physical assumption that may be incorr ect in some systems [ 7 , 19 ]. At this point, further investigation of the pr ocess of detachment would have to be carried out. In the following, we remain in the framework of the ‘Johnson paradigm’, and use the detachment condition (2.19) and equations based on it. W e will treat both the displacement-contr olled and load-controlled cases in the normal dir ection, but will confine ourselves to displacement control in the horizontal direction. 2.2.1. Adhesion for ce under load- contr olled conditions Under load-controlled conditions, the instability occurs at the contact radius at which the normal force is minimized. Thus, the condition of instability can be written as d F z /d a = 0. Dif ferentiating equation (2.22) with respect to a and using equation (2.21) we arrive at the condition 2 a 2 c , fl R 2 π γ a c , fl E ∗ − G ∗ E ∗ u (0)2 x − 3 π γ a c , fl E ∗ + G ∗ E ∗ u (0)2 x = 0, (2.27) or , in dimensionless variables (2.15) ˜ a 2 c , fl ˜ a c , fl − G ∗ 16 E ∗ ˜ u (0)2 x − ˜ a c , fl + G ∗ 24 E ∗ ˜ u (0)2 x = 0. (2.28) This equation determines the dependence of the critical radius ˜ a c , fl on the tangential displacement ˜ u (0) x . The dependence of the adhesion for ce on the tangential force can be determined by substituting ˜ a c , fl into equations (2.24)–(2.26). This dependence is shown in figur e 3 a (lower solid line). For ˜ F x = 0( o r ˜ u (0) x = 0), equations (2.24), (2.25) and (2.28) pr ovide the critical force ˜ F z (0) =− 1. Let us note that the dependence shown in figur e 3 a determines the critical tangential force for both positive and negative normal forces. In the case of the negative normal for ce, this critical value re ally corresponds to loss of ‘adhesive’ contact, as destr uction of the contact will lead to movement of the indenter away from the substrate. In the case of positive normal for ces, contact will not be lost at the critical value, only the continuity of the contact will be lost, which can be understood as propagation of a mode II (tangential) crack. The critical condition (2.19) does not differ entiate between these two cases, so the resulting dependences of F z on F x ar e equally valid for positive and negative F z , although the physical interpretation is dif fer ent. 8 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ 2.2.2. Adhesion under displacemen t- contr olled conditions For the pure normal contact, this mode is shown in figur e 2 a ; the detachment occurs at F z / F 0 = ˜ F z =− 0.5. The condition of instability is in this case formally given by d( d )/d a = 0. Thus, in the general case of superimposed normal and tangential loading, differ entiating (2.24) gives a 3 c , fg − G ∗ u (0)2 x 2 π γ a 2 c , fg − 2 π γ R 2 16 E ∗ = 0, (2.29) or , in dimensionless variables (2.15) ˜ a 3 c , fg − G ∗ 16 E ∗ ( ˜ u (0) x ˜ a c , fg ) 2 − 1 9 = 0. (2.30) This equation determines the dependence of the critical radius ˜ a c , fg on the tangential displacement ˜ u (0) x . For critical forces at the moment of detachment, we obtain ˜ F 2 x = 4 G ∗ E ∗ ˜ a 3 − 1 9 (2.31) and ˜ F z = ˜ a 3 − 2 3 . (2.32) From the two last equations, it follows ˜ F z = E ∗ 4 G ∗ ˜ F 2 x − 5 9 . (2.33) For the case E * = G *, the relationship between ˜ F z and ˜ F x under displacement control simplifies to ˜ F z = 1 4 ˜ F 2 x − 5 9 . (2.34) This dependence is shown in figure 3 a (upper solid line). Additionally , in figure 3 b the differ ences between the normal forces shown in figur e 3 a , ˜ F z , are shown as a function of normalized tangential for ce ˜ F x . At zero tangential for ce ˜ F x = 0, this differ ence is equal to ˜ F z (0) = ˜ F fg z (0) − ˜ F fl z (0) =− 5/9 − ( − 1) = 4/9. W ith increasing ˜ F x the value ˜ F z monotonically decreases. Note that the lower dependence in figur e 3 a (under load-controlled c onditions in the normal direction and displacement contr ol in the tangential direction) is well approximated by equation (2.34) when value ˜ F z shown in figure 3 b is close to zer o. At ˜ F x 1 both dependences shown in figure 3 a coincide and ar e described by equation (2.34). 3. Numerical pr ocedur e and c omparison with analytical r esults In the following, we r eproduce the above r esults numerically and use the developed numerical procedur e to extend them to a more complicated detachment condition. Let us first briefly describe the numerical procedur e for the case of normal adhesive contact. In the first step, the modified parabolic pr ofile g ( x ) (2.5) is indented by d into the elastic foundation shown in figure 1 b . After this, the position of the critical boundary springs (and thus the contact radius) is calculated using the condition (2.11). Given the indentation depth and the contact radius, the normal and tangential forces can be obtained by summing the forces of all springs in contact: F z = E ∗ x cont u z ( x i ) (3.1) and F x = G ∗ x cont u x ( x i ), (3.2) where u z ( x i )a n d u x ( x i ) are, r espectively , the normal and tangential displacements of individual springs at the coordinate x i . In a pur ely normal contact u x ( x i ) = 0, and F x = 0. When analysing the adhesive contact under displacement-controlled conditions, we displace the rigid indenter in the vertical direction step by step with a chosen discr etization z . The new configuration of contact after each step is calculated using the rule (2.11) for the springs at the boundary of the contact. If it happens that more than two springs are detached, we r eturn to the pr evious step and proceed further with a discretization step z /2 and, if necessary , decr ease it further until only one spring is lost on each side. This procedur e is continued up to the point of the instability . For load-controlled conditions, the contr olling parameter is the normal for ce F up .I ne a c hs t e p , F up is increased by an incr ement F , and the new equilibrium configuration of the contact is found. Similar 9 rsos.r oy alsocietypublishing.or g R. Soc. open sci. 4 : 161010 ................................................ to the pr ocedure for displacement contr ol, the incr ement of the force is decr eased if mor e than two springs are detached in one step. The r esults of numerical calculations with displacement-contr olled and load-controlled conditions for normal motion ar e presented together with analytical r esults in figure 2 . Since the numerical r esults coincide with the analytical ones, this provides some validation for the above numerical procedur e. The procedur e in the case of combined normal and tangential loading is basically the same as described above. The only differ ence is the use of a modified detachment condition l = u 2 x + u 2 z = l max . (3.3) In figure 3 a , the results of numerical calculations ar e shown along with analytical results pr esented in the previous section. 4. C onclusion W e performed analytical and numerical analysis of the adhesive contact between two elastic bodies with an axially symmetric gap profile under superimposed normal and tangential loading. The study was performed under the simplest assumption that the surface energy does not depend on the dir ection of detachment. However , the developed analytical method can be generalized straightforwar dly for more complicated adhesive interactions, as for example suggested in [ 23 ]. Under the above assumptions, the application of tangential force leads to a decrease of the normal adhesive for ce. W e considered dif ferent combinations of contr olled load and controlled displacement in both normal and tangential dir ections and derived for each case solutions in the appropriate dimensionless variables. In the case of mor e general adhesive interaction than assumed in this paper , it would further be inter esting to take into account the partial slip and frictional forces in the contact plane (as has been done for the special case of the Dugdale adhesive potential in [ 27 ]). Data acc essibilit y . No supporting data needed. All necessary algorithms ar e fully described in article. Authors’ c ontributions. V .L.P . proposed the idea of the article, performed the analytical investigation and wrote the text of the article; I.A.L. and A.E.F . carried out numerical analysis of the equations and performed numerical modelling. All authors gave final approval for publication. Competing in terests . W e declar e we have no competing interests. Fun d in g. 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