6,434 research outputs found
On the geometric nature of characteristic classes of surface bundles
Each Morita--Mumford--Miller (MMM) class e_n assigns to each genus g >= 2
surface bundle S_g -> E^{2n+2} -> M^{2n} an integer e_n^#(E -> M) :=
in Z. We prove that when n is odd the number e_n^#(E -> M) depends only on the
diffeomorphism type of E, not on g, M, or the map E -> M. More generally, we
prove that e_n^#(E -> M) depends only on the cobordism class of E. Recent work
of Hatcher implies that this stronger statement is false when n is even. If E
-> M is a holomorphic fibering of complex manifolds, we show that for every n
the number e_n^#(E -> M) only depends on the complex cobordism type of E.
We give a general procedure to construct manifolds fibering as surface
bundles in multiple ways, providing infinitely many examples to which our
theorems apply. As an application of our results we give a new proof of the
rational case of a recent theorem of Giansiracusa--Tillmann that the odd MMM
classes e_{2i-1} vanish for any surface bundle which bounds a handlebody
bundle. We show how the MMM classes can be seen as obstructions to low-genus
fiberings. Finally, we discuss a number of open questions that arise from this
work.Comment: 26 pages. v2: added examples to final section; v3: improved main
theorem for complex fiberings; v4: final version, to appear in Journal of
Topolog
Integrality in the Steinberg module and the top-dimensional cohomology of SL_n(O_K)
We prove a new structural result for the spherical Tits building attached to
SL_n(K) for many number fields K, and more generally for the fraction fields of
many Dedekind domains O: the Steinberg module St_n(K) is generated by integral
apartments if and only if the ideal class group cl(O) is trivial. We deduce
this integrality by proving that the complex of partial bases of O^n is
Cohen-Macaulay. We apply this to prove new vanishing and nonvanishing results
for H^{vcd}(SL_n(O_K); Q), where O_K is the ring of integers in a number field
and vcd is the virtual cohomological dimension of SL_n(O_K). The (non)vanishing
depends on the (non)triviality of the class group of O_K. We also obtain a
vanishing theorem for the cohomology H^{vcd}(SL_n(O_K); V) with twisted
coefficients V.Comment: 36 pages; final version; to appear in Amer. J. Mat
A stability conjecture for the unstable cohomology of SL_n Z, mapping class groups, and Aut(F_n)
In this paper we conjecture the stability and vanishing of a large piece of
the unstable rational cohomology of SL_n Z, of mapping class groups, and of
Aut(F_n).Comment: 18 pages. v2: final version, to appear in Algebraic Topology:
Applications and New Directions, AMS Contemporary Mathematics Serie
Comparison of SMAC, PISO, and iterative time-advancing schemes for unsteady flows
Calculations of unsteady flows using a simplified marker and cell (SMAC), a pressure implicit splitting of operators (PSIO), and an iterative time advancing scheme (ITA) are presented. A partial differential equation for incremental pressure is used in each time advancing scheme. Example flows considered are a polar cavity flow starting from rest and self-sustained oscillating flows over a circular and a square cylinder. For a large time step size, the SMAC and ITA are more strongly convergent and yield more accurate results than PSIO. The SMAC is the most efficient computationally. For a small time step size, the three time advancing schemes yield equally accurate Strouhal numbers. The capability of each time advancing scheme to accurately resolve unsteady flows is attributed to the use of new pressure correction algorithm that can strongly enforce the conservation of mass. The numerical results show that the low frequency of the vortex shedding is caused by the growth time of each vortex shed into the wake region
Internal computational fluid mechanics on supercomputers for aerospace propulsion systems
The accurate calculation of three-dimensional internal flowfields for application towards aerospace propulsion systems requires computational resources available only on supercomputers. A survey is presented of three-dimensional calculations of hypersonic, transonic, and subsonic internal flowfields conducted at the Lewis Research Center. A steady state Parabolized Navier-Stokes (PNS) solution of flow in a Mach 5.0, mixed compression inlet, a Navier-Stokes solution of flow in the vicinity of a terminal shock, and a PNS solution of flow in a diffusing S-bend with vortex generators are presented and discussed. All of these calculations were performed on either the NAS Cray-2 or the Lewis Research Center Cray XMP
Single-photon generation and simultaneous observation of wave and particle properties
We describe an experiment that generates single photons on demand and
measures properties accounted to both particle- and wave-like features of
light. The measurement is performed by exploiting data that are sampled
simultaneously in a single experimental run.Comment: The following article has been submitted to Proceedings of
"Foundations of probability and physics-3", Vaxjo, Sweden 2004. After it is
published, it will be found at http://proceedings.aip.org/ . 1 Reference was
added in version
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