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Software Package for the Development of Thermal Protection Systems for Spacecraft Descent into the Atmospheres of Planets

Solar system research, 2018-12, Vol.52 (7), p.578-589

2018

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How Particles in the Martian Atmosphere Influence the Thermal Protection Structure of the Descent Module EXOMARS-2

Solar system research, 2017-12, Vol.51 (7), p.628-638

2017

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Simulation of asteroid braking in the Earth atmosphere

Kompʹûternye issledovaniâ i modelirovanie (Online), 2013-12, Vol.5 (6), p.917-926

Golomazov, M. M.

2013

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Computational and theoretical investigation of Mars’s atmospheric impact on the descent module “Exomars-2018” under aerodynamic deceleration

Solar system research, 2016-12, Vol.50 (7), p.498-507

2016

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Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project

Solar system research, 2014-12, Vol.48 (7), p.541-548

2014

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On the boundary conditions on a shock wave for hypersonic flow around a descent vehicle

Solar system research, 2013-12, Vol.47 (7), p.520-527

2013

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On the Dynamics of Atmospheric Gas Filling the Interior of a Prospective Descent Module During Descent in the Atmosphere of Mars

Solar system research, 2020-12, Vol.54 (7), p.574-581

2020

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Study of Aerodynamics of a Prospective Descent Module Descending in the Atmosphere of Mars

Solar system research, 2019-12, Vol.53 (7), p.500-505

2019

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Numerical Study of Physical and Chemical Processes in the Shock Layer on the Trajectory of a Return Vehicle in the Atmosphere

Solar system research, 2019-12, Vol.53 (7), p.606-613

2019

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Program package for the computer-aided aerodynamic design system for descent vehicles in planetary atmospheres

Solar system research, 2012-12, Vol.46 (7), p.542-547

2012

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On the Use of Inflatable Decelerators in the Design of Spacecraft Intended for the Study of Venus

Solar system research, 2020-12, Vol.54 (7), p.595-602

2020

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Calculation of Radiation Heat Transfer in Problems of Flow past Bodies with Account for Heat-Shield Coating Mass Loss

Fluid dynamics, 2004-07, Vol.39 (4), p.633-641

2004

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Behavior of sonic lines in a shock layer behind a detached shock wave

Fluid dynamics, 1980-01, Vol.14 (4), p.588-590

1980

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Investigation of the flow fields in the region of interaction of a supersonic underexpanded jet with an obstacle

Fluid dynamics, 1982-01, Vol.17 (3), p.479-482

1982

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Hypersonic flow past evaporating bodies at an angle of attack

Fluid dynamics, 1984, Vol.19 (1), p.111-116

1984

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Pylephlebitis as a complication of acute appendicitis

Klinicheskaia khirurgiia, 1981-04 (4), p.72

Golomazov, M F

1981

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Supersonic dissociating gas flow past a blunt body at a finite angle of attack

U.S.S.R. computational mathematics and mathematical physics, 1971, Vol.11 (4), p.313-323

Golomazov, M.M.

1971

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Clinico-morphologic characteristics of the healing of suppurative wounds under the effects of dimethyl sulfoxide (experimental study)

Klinicheskaia khirurgiia, 1970-02, Vol.2, p.52

Golomazov, M F

1970

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Interaction of immersed jets with obstacles

Fluid dynamics, 1980-03, Vol.14 (5), p.759-761

1980

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Interaction of immersed jets with obstacles

Fluid dynamics, 1979-09, Vol.14 (5), p.759-761

1979

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Three-dimensional interaction of a freely expanding jet with obstacles

Fluid dynamics, 1982, Vol.17 (1), p.16-21

1982

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A numerical method of computing the three-dimensional flow past blunt bodies with a detached shock wave

U.S.S.R. computational mathematics and mathematical physics, 1975, Vol.15 (5), p.259-265

1975

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Causes of complications in acute appendicitis

Klinicheskaia khirurgiia, 1987 (4), p.53

1987

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Study of the effect of a strong blast of a gas from the surface on a hypersonic flow past blunt bodies

U.S.S.R. computational mathematics and mathematical physics, 1981, Vol.21 (4), p.204-215

1981

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Calculation of the flow about blunt bodies with a retracted shock wave in an equilibrium dissociating gas

U.S.S.R. computational mathematics and mathematical physics, 1964, Vol.4 (2), p.129-143

1964

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Software Package for the Development of Thermal Protection Systems for Spacecraft Descent into the Atmospheres of Planets

How Particles in the Martian Atmosphere Influence the Thermal Protection Structure of the Descent Module EXOMARS-2

Simulation of asteroid braking in the Earth atmosphere

Computational and theoretical investigation of Mars’s atmospheric impact on the descent module “Exomars-2018” under aerodynamic deceleration

Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project

On the boundary conditions on a shock wave for hypersonic flow around a descent vehicle

On the Dynamics of Atmospheric Gas Filling the Interior of a Prospective Descent Module During Descent in the Atmosphere of Mars

Study of Aerodynamics of a Prospective Descent Module Descending in the Atmosphere of Mars

Numerical Study of Physical and Chemical Processes in the Shock Layer on the Trajectory of a Return Vehicle in the Atmosphere

Program package for the computer-aided aerodynamic design system for descent vehicles in planetary atmospheres

On the Use of Inflatable Decelerators in the Design of Spacecraft Intended for the Study of Venus

Calculation of Radiation Heat Transfer in Problems of Flow past Bodies with Account for Heat-Shield Coating Mass Loss

Behavior of sonic lines in a shock layer behind a detached shock wave

Investigation of the flow fields in the region of interaction of a supersonic underexpanded jet with an obstacle

Hypersonic flow past evaporating bodies at an angle of attack

Pylephlebitis as a complication of acute appendicitis

Supersonic dissociating gas flow past a blunt body at a finite angle of attack

Clinico-morphologic characteristics of the healing of suppurative wounds under the effects of dimethyl sulfoxide (experimental study)

Interaction of immersed jets with obstacles

Interaction of immersed jets with obstacles

Three-dimensional interaction of a freely expanding jet with obstacles

A numerical method of computing the three-dimensional flow past blunt bodies with a detached shock wave

Causes of complications in acute appendicitis

Study of the effect of a strong blast of a gas from the surface on a hypersonic flow past blunt bodies

Calculation of the flow about blunt bodies with a retracted shock wave in an equilibrium dissociating gas

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