Separation of chemical elements in the discharge channel of an inductive plasma gun

Сахаров, В. И.

doi:10.1134/s0015462810040149

Cited by 1 publication

(2 citation statements)

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“…The corresponding equation for determining the tangential component of the curl electric ¦eld and boundary condition for this equation are given in [7,8] where the §ow of the equilibrium air plasma was considered.…”

Section: Results Of Numerical Investigations Of the Flow Around The Mmentioning

confidence: 99%

“…The study was carried out within a wide range of supersonic modes of WTs: air §ow rates, values of the power contributed in plasma, reverse pressures in decompression chambers, and sizes of outlet cross sections and sonic and supersonic nozzles. The technology of calculation of such §ows is based on a software system of numerical integration of Navier Stokes equations and special programs-generators which include data bases for thermodynamic and transfer properties of individual gaseous substances (HIGHTEMP) created in the Institute of Mechanics MSU [8].…”

Section: Introductionmentioning

confidence: 99%

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A blunted cone in a supersonic high-enthalpy nonequilibrium air flow

Сахаров

Shtapov

Vasilevskiy

et al. 2015

Progress in Flight Physics – Volume 7

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A calculation and experimental study was conducted with the §ow, heat §ux, and pressure distributions over the front and side surfaces of a blunt cone in a nonequilibrium high-enthalpy (h 0 = 25 MJ/kg) supersonic (M = 4) air §ow. The experiments were performed in a VAT-104 wind tunnel (WT), TsAGI. The nose part of the model with a small-radius nose R w = 10 mm and half angle θ = 10 • was inside the ¤Mach cone¥ of the underexpanded jet §owing out from the WT nozzle. Numerical and experimental results are in good agreement.

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Section: Results Of Numerical Investigations Of the Flow Around The Mmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%