2,336 research outputs found

    Pressure distributions on three different cruciform aft-control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 2: Clipped delta tail

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    Pressure coefficients were obtained in the Langley Unitary Plan wind tunnel for a wingless missile with a clipped delta tail. The angle of attack was varied from -4 deg to 20 deg, model roll angle was varied from 0 deg to 90 deg in 22.5 deg increments, and tail deflections were 0 deg to - 15 deg. The pressures were measured on two adjacent tail surfaces using 91 pressure orifices per tail surface. Results are presented in plotted and tabular form

    Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 3: Cranked tail

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    The results of pressure distribution tests are presented without analysis. The test Reynolds number used was 6.6. x 10 to the 6th power per meter

    Vapor-screen technique for flow visualization in the Langley Unitary Plan Wind Tunnel

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    The vapor-screen technique for flow visualization, as developed for the Langley Unitary Plan Wind Tunnel, is described with evaluations of light sources and photographic equipment. Test parameters including dew point, pressure, and temperature were varied to determine optimum conditions for obtaining high-quality vapor-screen photographs. The investigation was conducted in the supersonic speed range for Mach numbers from 1.47 to 4.63 at model angles of attack up to 35 deg. Vapor-screen photographs illustrating various flow patterns are presented for several missile and aircraft configurations. Examples of vapor-screen results that have contributed to the understanding of complex flow fields and provided a basis for the development of theoretical codes are presented with reference to other research

    Allocation of Ice Cream Distribution Costs

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    Skeleton Cave, Leigh Woods, Bristol

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    An account is given of the discovery and excavation of this small cave in the 1960s. It is recorded that archaeological finds were made, but of these, only a single human mandible can now be traced. Radiocarbon dating shows the specimen to be early Neolithic in age; a metrical analysis was less conclusive.http://www.ubss.org.uk/resources/proceedings/vol27/UBSS_Proc_27_2_197-209.pd

    LpL^p continuity of eigenprojections for 2-d Dirichlet Laplacians under perturbations of the domain

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    We generalise results by Lamberti and Lanza de Cristoforis (2005) concerning the continuity of projections onto eigenspaces of self-adjoint differential operators with compact inverses as the (spatial) domain of the functions is perturbed in R2\mathbb{R}^2. Our main case of interest is the Dirichlet Laplacian. We extend these results from bounds from H01H_0^1 to H01H_0^1 to bounds from LpL^p to LpL^p, under the assumption that (−Δ−1−z)−1(-\Delta^{-1}-z)^{-1} is LpL^p bounded when zz lies outside of the spectrum of −Δ−1-\Delta^{-1}. We show that this assumption is met if the initial domain is a square or a rectangle.Comment: 27 pages, 2 figure

    Long-range interactions for He(nSn S)--He(n′S)(n' S) and He(nSn S)--He(n′P)(n' P)

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    The energetically lowest five states of a helium atom are: He(11S1^1S), He(23S2^3S), He(21S2^1S), He(23P2^3P), and He(21P2^1P). Long-range interaction coefficients C3C_3, C6C_6, C8C_8, C9C_9, and C10C_{10} for all S−SS-S and S−PS-P pairs of these states are calculated precisely using correlated wave functions in Hylleraas coordinates. Finite nuclear isotope mass effects are included
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