channel of 
A numerical model of the turbulent boundary layers in the gas dynamic channel of a supersonic MHD generator is constructed.


The threedimensional viscous compressible flow in the interblade channel of a turbomachine blade row is examined.


Heat and mass transfer associated with lowvelocity vapor flow in the plane channel of a thermal protection system of the radiat


Below, a flow model and a method of calculating the flow in a narrow plane channel of finite length in the presence of evaporation or sublimation on one wall induced by radiativeconductive heat transfer from the other hot wall are proposed.


Modeling the unsteady heat and mass transfer in the vapor outlet channel of a radiativeevaporative thermal protection system


Analytical study of supersonic isentropic flow in a channel of constant cross section and an adjacent laval nozzle.


Flow in both a channel of constant cross section and an adjacent Laval nozzle with a corner point is considered.


The coupled boundaryvalue problem of nonstationary heat and mass transfer within the outer thermal insulation layer and the vapor outlet channel of a combined radiativeevaporative thermal protection system is formulated.


The regime obtained describes the flow in the stream core of the channel of a modern quasisteady heavycurrent plasma accelerator outside thin nearelectrode layers.


Unsteady flow of a twophase disperse medium from a cylindrical channel of finite dimensions into the atmosphere


Within the framework of the mechanics of heterogenous media, the flow of a mixture of highpressure gas and an initially closepacked disperse phase from a cylindrical channel of finite dimensions into the atmosphere is investigated numerically.


The variational problem of optimizing the energy supplied to the discharge channel of a pulsed water jet in order to maximize the mean jet outflow velocity is considered.


Effect of water density inversion on the planeparallel flow and heat transfer in a channel of constant width


The convective mass (heat) transfer domain is a cylindrical channel of arbitrary cross section.


The results of calculating the air and argon plasma flow and temperature field in the discharge channel of a 100 kW induction plasmatron are given.


The radiation gasdynamic processes in the channel of an air laser plasma generator operating at atmospheric pressure are analyzed.


The drag of circular cylinders of different size and mass in a circulationfree water flow in a plane channel of rectangular crosssection was studied in the transverse selfoscillation regime.


The structure of the flow in an inlet with threedimensional compression and an adjoining channel of rectangular crosssection is experimentally investigated for the external flow parameters M∞ = 4 and Re ≈ 52 · 106 1/m.


On the basis of numerical modeling, the formation of an unsteady shock wave induced by a condensation shock in a rarefaction wave moving in the highpressure channel of a shock tube filled with moist air is demonstrated.


A highenergy channel of C3H6 formation upon IR multiphoton excitation of C3H5Ge(CH3)3

