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17 PRIMA 2013 AbstractsSpecial Session 8Hyperbolic Conserv<strong>at</strong>ion Laws and Rel<strong>at</strong>edApplic<strong>at</strong>ionsSome counterexamples in the theory of conserv<strong>at</strong>ionlawsAlberto BressanPennsylvania St<strong>at</strong>e University, USAbressan@m<strong>at</strong>h.psu.eduThe first part of the talk is concerned with sticky particlemodels in two space dimensions. Examples of Cauchyproblems can be constructed with two and with zero solutions,respectively. Similar ideas apply to the equ<strong>at</strong>ionsof pressureless gases in two space dimensions, with L ∞initial d<strong>at</strong>a.The second set of examples concern the p-system of isentropicgas dynamics. For initial d<strong>at</strong>a with large totalvari<strong>at</strong>ion, one can arrange repe<strong>at</strong>ed wave-front interactionsin such a way th<strong>at</strong> the total strength of all wavefronts becomes arbitrarily large.Nonlinear mixed type equ<strong>at</strong>ions arisen inMach reflectionShuxing ChenFudan University, Chinasxchen@fudan.edu.cnIn the study of Mach reflection we find a kind of nonlinearmixed type equ<strong>at</strong>ions. The solvability of the generalizedTricomi problem of the mixed type equ<strong>at</strong>ion leads thestability of corresponding Mach configur<strong>at</strong>ion.Self-similar vortex spiral solutions of the 2dincompressible Euler Equ<strong>at</strong>ionsVolker EllingUniversity of Michigan, Ann Arbor, USAvelling@umich.eduVortex spirals are ubiquitous in fluid flow, for example asturbulent eddies or as trailing vortices <strong>at</strong> aircraft wings.However, there are few proofs of existence for any of thecommon fluid models. We consider solutions of the incompressibleEuler equ<strong>at</strong>ions th<strong>at</strong> have vorticity str<strong>at</strong>ifyinginto algebraic spirals. The solutions are selfsimilar:velocity v(t, x) = t m−1 v(t −m x), for similarity exponent1< m < ∞. Selfsimilar flows are special solutions of the2full initial-value problem, but obtained by solving moretractable boundary value problems. The key to the existenceproof is an coordin<strong>at</strong>e change which is implicit,depending on the a priori unknown solution. We willalso discuss the importance of the program for showingnon-uniqueness in the initial-value problem for the 2d incompressibleEuler solutions.Some results about compressible Oldroyd-BDaoyuan FangZhejiang University, Chinadyf@zju.edu.cnIn this talk, I will show some results about the compressibleOldroyd-B model, which is the joint work withRuizhao Zi. For such medel, we proved th<strong>at</strong> the systemadmits a unique local strong solution with initial densityvanishes from below, and give a blow-up criterion; Inthe framework of critical spaces, we establish the globalsolutions if the initial d<strong>at</strong>a and coupling constant are sufficientlysmall. We also proved th<strong>at</strong> as the Mach numbertends to zero, the global solution converges to the solutionto the corresponding incompressible model in somefunction spaces,and obtained a kind of the converge r<strong>at</strong>es.Shock reflection and von Neumann conjecturesMikhail FeldmanUniversity of Wisconsin-Madison, USAfeldman@m<strong>at</strong>h.wisc.eduWe discuss shock reflection problem for compressible gasdynamics, and von Neumann conjectures on transitionbetween regular and Mach reflections. Then we describerecent results on existence of regular reflection solutionsfor potential flow equ<strong>at</strong>ion up to the detachment angle,and discuss some techniques. The approach is to reducethe shock reflection problem to a free boundary problemfor a nonlinear equ<strong>at</strong>ion of mixed elliptic-hyperbolic type.Open problems will also be discussed. The talk will bebased on the joint work with Gui-Qiang Chen.Normal forms and a Burgers-Hilbert equ<strong>at</strong>ionJohn K. HunterUniversity of California, Davis, USAjkhunter@ucdavis.eduThe Burgers-Hilbert equ<strong>at</strong>ion arises as a model equ<strong>at</strong>ionfor the motion of a vortex p<strong>at</strong>ch or vorticity discontinuityin a two-dimensional, inviscid, incompressible fluid flow,and describes the effect of nonlinear steepening on an interfaceor wave th<strong>at</strong> oscill<strong>at</strong>es <strong>at</strong> a constant backgroundfrequency. For small amplitudes, these oscill<strong>at</strong>ions delaywave breaking. We will explain how non-standardnormal form methods can be used to prove an enhancedlife-span of small smooth solutions of the Burgers-Hilbertequ<strong>at</strong>ion in comparison with the inviscid Burgers equ<strong>at</strong>ion.These normal form methods can be applied to otherquasilinear wave equ<strong>at</strong>ions, for which the Burgers-Hilbertequ<strong>at</strong>ion provides a useful test case. This is joint workwith M. Ifrim, D. T<strong>at</strong>aru, and D. Wong.Incompressible limit of the non-isentropicideal magnetohydrodynamic equ<strong>at</strong>ionsSong JiangInstitute of Applied Physics and Comput<strong>at</strong>ional M<strong>at</strong>hem<strong>at</strong>ics,Chinajiang@iapcm.ac.cnWe first give a short review of results on the low Machnumber limit for the compressible magnetohydrodynamicequ<strong>at</strong>ions. Then, we study the incompressible limit of thecompressible non-isentropic ideal magnetohydrodynamicequ<strong>at</strong>ions with general initial d<strong>at</strong>a in the whole space IR d(d = 2, 3), and establish the existence of classic solutionson a time interval independent of the Mach number. Finally,by deriving uniform a priori estim<strong>at</strong>es, we obtainthe convergence of the solution to th<strong>at</strong> of the incompressiblemagnetohydrodynamic equ<strong>at</strong>ions as the Mach numbertends to zero.(joint-work with Q.C. Ju and F.C. Li)The Cauchy problem to the Kazhikhov-Vaigant model in compressible flowQuansen JiuCapital Normal University, Chinajiuqs@mail.cnu.edu.cnIn this talk, we will present some recent progresses ofthe global well-posedness of the Cauchy problem to the

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