Numerical computation of flow past a scalariform cone
Numerical computation of uniform flow past scalariform circular cone immersed in supersonic stream of ideal gas
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Numerical computation of uniform flow past scalariform circular cone immersed in supersonic stream of ideal gas
Convective heat transfer and pressure distribution measurements on lifting blunt cone reentry body
Local flow conditions over hemispherically blunted 25 deg cone for shallow reentry trajectory
Tabulated values of ratio of cone surface pressure-pressure at shock
Laminar and turbulent boundary layer flow in ablating cones in hypervelocity flight
Static pitching moment coefficient determination from location of center of pressure in right circular cone, using Newtonian impact mechanics
Laminar and turbulent boundary layer flow in ablating cones in hypervelocity flight
High amplitude, dynamic stability characteristics of blunt 10-degree cones
Cone radiometer evaluation, and its application as measuring apparatus of incidence light flux
Pressure distribution measurements on cones in symmetrical incompressible flow, with and without influence of wake
Transonic flutter of simple thin truncated-cone panels
Aerodynamic characteristics and pressure distributions of spherically blunted 25 degree cone investigated in nitrogen at Mach 20
Shear lag effect on stress distribution in stiffened shells, and stress analysis of cone frustums and segments
Nose bluntness and cone angle effects on base pressure and heating in laminar hypersonic flow regime, using free flight telemetry technique
The aeroelastic stability of a tail cone thruster fan was analyzed for three structural modes and various nodal diameter patterns. Computational fluid dynamics modeling with blade vibrations was used in the analyses performed at design (peak-efficiency) and two near-stall conditions at the design rotational speed. Aerodynamic damping was used to assess flutter since this integrally bladed rotor design will have minimal structural damping. Aerodynamic damping was found to be low at the design condition. For the first mode, aerodynamic damping was seen to decrease towards stall, vanishing for a zero nodal diameter pattern. Further decrease in mass flow led to negative aerodynamic damping (flutter) for the first and second nodal diameters in the near stall condition. The flowfield at this lowest mass flow rate exhibited some additional unsteadiness at higher frequency. The sensitivity of results to time step and amplitudes of vibration was examined and found to be very satisfactory. The largest uncertainty in the results comes from the observed sensitivity of the aerodynamic damping to details of the variation of grid deformations in the blade passage mesh from the blade passage to the boundaries. For the parametric variations analyzed, the calculated aerodynamic damping is lower if the grid deformations near the blade surface are higher. Further work is needed to understand the cause of this sensitivity and find possible solutions to reduce the effects on flutter predictions.
Angle resolved photoemission spectroscopy (ARPES) study on TlBiTe2 and TlBiSe2 from a Thallium-based III-V-VI2 ternary chalcogenides family revealed a single surface Dirac cone at the center of the Brillouin zone for both compounds. For TlBiSe{sub 2}, the large bulk gap ({approx} 200meV) makes it a topological insulator with better mechanical properties than the previous binary 3D topological insualtor family. For TlBiTe{sub 2}, the observed negative bulk gap indicates it as a semi-metal, rather than a narrow gap semi-conductor as conventionally believed; this semi-metality naturally explains its mysteriously small thermoelectric figure of merit comparing to other compounds in the family. Finally, the unique band structures of TlBiTe{sub 2} also suggests it as a candidate for topological superconductors.
Quantum states with geometric duals are known to satisfy a stricter set of entropy inequalities than those obeyed by general quantum systems. The set of allowed entropies derived using the Ryu-Takayanagi (RT) formula defines the Holographic Entropy Cone (HEC). These inequalities are no longer satisfied once general quantum corrections are included by employing the Quantum Extremal Surface (QES) prescription. Nevertheless, the structure of the QES formula allows for a controlled study of how quantum contributions from bulk entropies interplay with HEC inequalities. In this paper, we initiate an exploration of this problem by relating bulk entropy constraints to boundary entropy inequalities. In particular, we show that requiring the bulk entropies to satisfy the HEC implies that the boundary entropies also satisfy the HEC. Further, we also show that requiring the bulk entropies to obey monogamy of mutual information (MMI) implies the boundary entropies also obey MMI.