Urn Models and Beta-splines

Some insight into the properties of beta-splines is gained by applying the techniques of urn models. Urn models are used to construct beta-spline basis functions and to derive the basic properties of these blending functions and the corresponding beta-spline curves. Only the simple notion of linear geometric continuity and with the most elementary beta parameter are outlined. Non-linear geometric continuity leads to additional beta parameters and to more complicated basis functions. Whether urn models can give us any insight into these higher order concepts still remains to be investigated

Threaded pilot insures cutting tool alignment

Threaded pilot allows machining of a port component, or boss, after the reciprocating hole has been threaded. It is used to align cutting surfaces with the boss threads, thus insuring precision alignment

Pion LINAC as an Energy-Tagged Neutrino Source

The energy spectrum and flux of neutrinos from a linear pion accelerator are calculated analytically under the assumption of a uniform accelerating gradient. The energy of a neutrino from this source reacting in a detector can be determined from timing and event position information.Comment: 16 pages, 4 figures. Replacement of Section II.D and minor corrections elsewhere. The basic point and conclusions of the paper are unchanged. Phys. Rev. ST Accel. Beams 11,124701 (2008); Erratum submitte

On the interaction of a small number of transverse and longitudinal modes in a plasma

Equations for interaction of large amplitude transverse and longitudinal waves in Vlasov plasm

Design of two-dimensional sharp-edged-throat supersonic nozzle with boundary-layer correction

Computer program accounts for effective nozzle geometry changes due to boundary layer displacement thickness. Program input and output are discussed

Oil pollution detection and monitoring from space using Skylab

There are no author-identified significant results in this report

On the structure of the BBGKY hierarchy for a Boltzmann gas

Structure of BBGKY hierarchy for Boltzmann gas and particle distribution

SN1987A - a Testing Ground for the KARMEN Anomaly

We show, that SN1987A can serve as an astrophysical laboratory for testing the viability of the assertion that a new massive neutral fermion is implied by the KARMEN data. We show that a wide range of the parameters characterizing the proposed particle is ruled out by the above constraints making this interpretation very unlikely.Comment: 12 pages, 1 eps figure embedded, to appear in Phys. Lett.

Quantized Rabi Oscillations and Circular Dichroism in Quantum Hall Systems

The dissipative response of a quantum system upon a time-dependent drive can be exploited as a probe of its geometric and topological properties. In this work, we explore the implications of such phenomena in the context of two-dimensional gases subjected to a uniform magnetic field. It is shown that a filled Landau level exhibits a quantized circular dichroism, which can be traced back to its underlying non-trivial topology. Based on selection rules, we find that this quantized circular dichroism can be suitably described in terms of Rabi oscillations, whose frequencies satisfy simple quantization laws. Moreover, we discuss how these quantized dissipative responses can be probed locally, both in the bulk and at the boundaries of the quantum Hall system. This work suggests alternative forms of topological probes in quantum systems based on circular dichroism.Comment: 7 pages, including 3 figures and Appendi

Experimental investigation of hypersonic buzz on a high cross-range shuttle configuration

A wind tunnel investigation has been conducted to determine the nature of an unsteady hypersonic flow phenomenon, often referred to as hypersonic buzz, on a 1:100 scale model representative of a high cross-range shuttle configuration. The tests, conducted in helium at a nominal Mach number of 17.5, were specifically directed at obtaining a better understanding of the character of the hypersonic flow field in the vicinity of a deflected control surface. Power spectral densities and root mean squared values of surface pressure fluctuations are presented along with observations made from high speed motion pictures, schlieren and oil flow photographs. Flap deflections of 0, 20, 30, 35, 40 and 60 deg were tested at various angles of attack from 0 deg to 37 deg. It is quite clear from these tests that, under certain conditions, extremely unstable hypersonic flow patterns are formed