2,672 research outputs found

    Intertwining of simple characters in GL(n)

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    Let FF be a non-Archimedean local field and let GG be the general linear group G=GLn(F)G = \text{\rm GL}_n(F). Let θ1\theta_1, θ2\theta_2 be simple characters in GG. We show that θ1\theta_1 intertwines with θ2\theta_2 if and only if θ1\theta_1 is endo-equivalent to θ2\theta_2. We also show that any simple character in GG is a GG-type.Comment: 7 page

    Tame multiplicity and conductor for local Galois representations

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    Let FF be a non-Archimedean locally compact field of residual characteristic pp. Let σ\sigma be an irreducible smooth representation of the absolute Weil group \Cal W_F of FF and \sw(\sigma) the Swan exponent of σ\sigma. Assume \sw(\sigma) \ge1. Let \Cal I_F be the inertia subgroup of \Cal W_F and \Cal P_F the wild inertia subgroup. There is an essentially unique, finite, cyclic group Σ\varSigma, of order prime to pp, so that \sigma(\Cal I_F) = \sigma(\Cal P_F)\varSigma. In response to a query of Mark Reeder, we show that the multiplicity in σ\sigma of any character of Σ\varSigma is bounded by \sw(\sigma).Comment: Revised version with further detai

    Langlands parameters for epipelagic representations of GLn\text{\rm GL}_n

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    Let FF be a non-Archimedean local field. An irreducible cuspidal representation of GLn(F)\text{\rm GL}_n(F) is epipelagic if its Swan conductor equals 1. We give a full and explicit description of the Langlands parameters of such representations.Comment: 25 page

    Cycles in the chamber homology of GL(3)

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    Let F be a nonarchimedean local field and let GL(N) = GL(N,F). We prove the existence of parahoric types for GL(N). We construct representative cycles in all the homology classes of the chamber homology of GL(3).Comment: 45 pages. v3: minor correction

    Status of linear boundary-layer stability and the e to the nth method, with emphasis on swept-wing applications

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    The-state-of-the-art for the application of linear stability theory and the e to the nth power method for transition prediction and laminar flow control design are summarized, with analyses of previously published low disturbance, swept wing data presented. For any set of transition data with similar stream distrubance levels and spectra, the e to the nth power method for estimating the beginning of transition works reasonably well; however, the value of n can vary significantly, depending upon variations in disturbance field or receptivity. Where disturbance levels are high, the values of n are appreciably below the usual average value of 9 to 10 obtained for relatively low disturbance levels. It is recommended that the design of laminar flow control systems be based on conservative estimates of n and that, in considering the values of n obtained from different analytical approaches or investigations, the designer explore the various assumptions which entered into the analyses

    Induced representations of locally profinite groups

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