Add to ORKGThe creation of investigation effective and economic analytical and numeric methods of the viscous gas hupersonic flow is the aim of the paper. As a result analytical solutions and formulae have been obtained. Effective and economic numerical algorithms have been created. The influence of determining parameters on thermal force loading of flowed bodies has been investigatedAvailable from VNTIC / VNTIC - Scientific & Technical Information Centre of RussiaSIGLERURussian Federatio
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
Communications to : 14th international conference on numerical methods in fluid mechanics, Bangalore...
The law of plane cross sections for the three-dimensional boundary layer on the thin wings of small ...
The flow of the compressible gas is investigated by means of the developed finite-difference compute...
A process of the gas flow in a shock layer is investigated in the paper aiming at the development of...
Numerical modelling problems of three-dimensional flows on the base of Navier - Stoks equations are ...
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
Subject of inquiry: hypersonic flow about blunt-nosed bodies under transient condition from free-mol...
Subject of inquiry: supersonic viscous impact layer. The aim of the work is to develop efficient num...
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
The purpose of this study is to model hypersonic flow around blunt body especially in atmospheric re...
The task about supersonic uneven flow of the blunt lenghtened bodies at different flow conditions ha...
The study considers the solution of a number of problems of supersonic and hypersonic gas dynamics u...
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
In the design of an hypersonic configuration heat-transfer plays an essential role. For computations...
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
Communications to : 14th international conference on numerical methods in fluid mechanics, Bangalore...
The law of plane cross sections for the three-dimensional boundary layer on the thin wings of small ...
The flow of the compressible gas is investigated by means of the developed finite-difference compute...
A process of the gas flow in a shock layer is investigated in the paper aiming at the development of...
Numerical modelling problems of three-dimensional flows on the base of Navier - Stoks equations are ...
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
Subject of inquiry: hypersonic flow about blunt-nosed bodies under transient condition from free-mol...
Subject of inquiry: supersonic viscous impact layer. The aim of the work is to develop efficient num...
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
The purpose of this study is to model hypersonic flow around blunt body especially in atmospheric re...
The task about supersonic uneven flow of the blunt lenghtened bodies at different flow conditions ha...
The study considers the solution of a number of problems of supersonic and hypersonic gas dynamics u...
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
In the design of an hypersonic configuration heat-transfer plays an essential role. For computations...
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
Communications to : 14th international conference on numerical methods in fluid mechanics, Bangalore...
The law of plane cross sections for the three-dimensional boundary layer on the thin wings of small ...