Spatial distribution of CO2 dimers in axisymmetric gas jets expanding in a vacuum

Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 1, pp. 56–62, January–February, 1989.     

Thermal effect of a freely expanding gas jet on a flat plate

An experimental investigation was made into the thermal effect of a single gas jet on a plate at Mach numbers of the nozzles in the range 2–6.1, specific heat ratio = 1.4, total pressure difference up to 6·10⁷, gas temperature 450–520 °K in the forechamber, and pressure in the forechamber (10–20)· 10⁵ Pa. The proposed dimensionless numbers made it possible to obtain generalized dependences of the distribution of the heat flux to the plate on the conditions of the problem. A method of approximate calculation of the heat fluxes is proposed.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 119–126, July–August, 1981.     

Formation of a jet of gas outflowing into evacuated space

Unsteady outflow from a sonic nozzle with off-design factor 4 · 10⁸ at an ambient pressure of 2 · 10^?5 mm Hg is studied by means of the absorption of an electron beam. The motion laws of the front of the outflowing gas and other characteristic regions of the outflow are studied. A comparison to the results of other works clarifies the features of outflow with high offdesign factors. An equation is obtained describing the motion of the front of outflowing gas along the flow axis. Results are presented in generalized similitude parameters.     

Numerical calculations for two-phase jet flow of a mixture of pulverized-coal and gas

In this paper, Euler-Lagrange type equations are used to describe the jet flow of a mixture of pulverized-coal and gas, which is an unsteady axisymmetric two-phase flow. By means of the finite-difference method, the coal particle's distribution, velocity and trajectory in the flow field are obtained. The coal particles are represented by a finite number of computational particles. Each particle's diameter is randomly assigned according to a given distribution. The states of the computational particles are different from each other. Turbulence is accounted for in a stochastic model. Explicit time-splitting scheme is used to calculate the strongly coupling interphase term. The numerical results are reasonable. The comparison between the numerical results and the experiment data for the case of the oil droplet injection shows good agreement. This numerical technique can be extended to the calculation of other two-phase flows of dilute particles or a droplet system. Mr. Mei Renwei also participated in the work of this paper.     

Motion of a gas mixture through a porous medium with sorption

Solutions are investigated of a system of linear partial differential equations describing the motion of a gaseous (liquid) mixture through an undeformable homogeneous porous medium with sorption at interfaces between gaseous (liquid) and solid phases, the kinetics of which are described by a linear equation. If the porous medium consists of spherical granules, the problem is solved in quadratures. For the case of symmetric granules with arbitrary symmetry parameter, various approximate solutions are obtained; first and central moments are used as criteria for the accuracy of the approximations.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 95–100, September–October, 1970.     

Flow characteristics of slot jet impingement on a wedge

An experimental investigation is made to study the flow characteristics of slot jet impingement on a wedge whose included angle is 90 degrees. The aim of this investigation is to study the characteristics of the flow field near the wedge surface for various parameters. The different parameters like, jet velocity, slot width, distance of wedge vertex from the jet exit and the inclination of the wedge to jet axis are systematically varied to see their effect on the flow field. The flow field near the wedge vertex is similar to stagnation point flow. Far away from the vertex, the flow field is like that of wall jet. Near the vertex, very large variations of static pressure are observed in streamwise and transverse directions. This is due to large streamwise curvature and stagnation of flow. The transverse pressure gradient slowly decays in the streamwise direction, as a result, the velocity profiles are different from the similarity profiles of stagnation point flow and wall jet in the respective regions. Experiments are conducted for slot widths of 10 mm, 15 mm and 30 mm each for the distance between slot and wedge vertex of 80 mm, 120 mm and 240 mm. The static pressure and velocity profiles are measured by calibrated disk type static pressure probe and pitot tube respectively at various streamwise locations.Es wurde eine experimentelle Studie über die Strömmungscharakteristiken eines auf einem rechtwinkligen Keil auftretenden Spaltstrahls durchgeführt. Das Ziel dieser Untersuchungen ist die Studie des Strömungsverhaltens in Keilnähe, in Abhängigkeit verschiedener Parameter wie Strahlgeschwindigkeit, Spaltbreite, Entfernung der Keilspitze und Winkel zwischen Strahlachse und Keil. Diese Parameter werden systematisch variiert um deren Einfluß auf das Strömungsverhalten zu bestimmen. Die Strömung an der Keilspitze ist ähnlich der Staupunktströmung. Weit hinter der Spitze gleicht das Strömungsfeld dem eines auf einer Wand auftreffenden Strahls. In Nähe der Keilspitze sind die Änderungen des statischen Drucks in Strömungsrichtung und quer zur Strömung groß. Grund dafür sind die starke Krümmung der Strömung und die Stagnation der Strömung. Der Druckgradient in Querrichtung nimmt langsam in Strömungsrichtung ab, daher unterscheiden sich die Geschwindigkeitsprofile von den Ähnlichkeitsprofilen der Staupunktströmung und des Wandstrahls in den jeweiligen Bereichen. Die Versuche wurden für Spaltbreiten von 10, 15 und 30 mm und Keilentfernungen von 80, 120 und 240 mm durchgeführt. Der statische Druck und die Geschwindigkeitsprofile wurden mit kalibrierten scheibenförmigen Drucksonden bzw. einer Pitot-Sonde an verschiedenen Orten gemessen.     

Three-dimensional interaction of a freely expanding jet with obstacles

A numerical scheme is proposed for calculating the steady three-dimensional flow in the subsonic and transonic regions of interaction of a freely expanding jet and an infinite flat obstacle at angles of attack up to 20 ° and the end of a cylinder placed relative to the jet axis at a distance up to ten nozzle radii. Results of calculations are given.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 22–27, January–February, 1981.We thank A. P. Zyuzin for making a number of calculations.     

Population inversion and radiation density in a Q-switched CO2 laser

The mechanism of lasing in a steady-state CO₂ laser has been investigated in [1–3]. In this paper we present a numerical analysis of the processes which occur in a CO₂ laser when the resonator is rapidly Q-switched. It is shown that the transition of the laser into the state with a new Q has an oscillatory form.Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 6, pp. 18–23, November–December, 1972.We wish to thank R. I. Soloukhin for his interest and help.     

Large eddy simulation of a slot jet impinging on a convex surface

A large eddy simulation is used to simulate flow and heat transfer in a turbulent plane jet with two distances from the jet-exit to impingement corresponding to twice and ten times the slot nozzle width. The resolved different unsteady vortex motions of the jet shear layers are studied and shown to have an important influence on heat transfer at the wall. They are used to explain existence of the second peak in Nusselt number for the case corresponding to twice the slot nozzle width. The predicted average surface Nusselt number profiles exhibit good agreement with experiments.     

Numerical modeling of jet flow in a slot channel in the transition regime

Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 6, pp. 108–112, November–December, 1991.     

Inverted population of Co2 molecules in expanding gas streams

The system of equations of hydrodynamics, which describes the process of escape of the mixtures CO₂ + N₂ + He, H₂O from a nozzle, is solved numerically in conjunction with the equations of the kinetics of the excitation of the vibrational degrees of freedom of the molecules. It is found that an inverted population of the CO₂ molecules with respect to the transition [00 °1] – [10 °0], is produced under certain conditions at the exit from the nozzle. The magnitude of the inversion depends both on the nozzle configuration and on the initial values of the gas temperature and pressure. It is shown that for a specified nozzle configuration there exist optimal values of these parameters, at which the inverted population of the CO₂ molecules reaches approximately 10¹⁵ cm^–3.Translated from Zhumal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 5, pp. 24–34, September–October, 1971.