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Инженерно-физический журнал, 2000, Том 73, No.1

Главная страница / Издания академии / Научные журналы

Инженерно-физический журнал, 2000, Том 73, No.1


Издатель: Институт тепло- и массообмена имени А.В. Лыкова НАН Беларуси, Минск, Беларусь

Volume 73, Number 1; January--February, 2000

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Foreword. pp. 1--3

Yu.V. Polezhaev
Will There or Will There not be a Hypersonic Airplane? pp. 5--10

S.V. Reznik
Mathematical Models of Radiative-Conductive Heat Exchange in Heat-Shield Materials of Shuttle Space Transportation Systems. pp. 11--25

V. S.Dozhdikov, V.A. Petrov
Radiation Characteristics of Heat Protective Materials of the Buran Orbital Spacecraft. pp. 26--30

S.T. Surzhikov
Two-Component Radiation-Gasdynamic Model of a Turbulent Fireball. pp. 31--38

K.B. Isaev, V.V. Kartuzov, A.K. Lapteva
Classification and Database of Thermophysical Characteristics of Heat Protective Materials. pp. 39--43

A.P. Kuryachii
Theoretical Modeling of Systems of Combined Thermal Protection. pp. 44--51

G.N. Isakov
Theoretical Principles of Design of Multilayer Swelling Heat Protection with Assigned Properties. pp. 52--60

V.I. Zinchenko, V.V. Nesmelov, G.F. Kostin
Heat and Mass Transfer in the Destruction of Thermal Protective Materials with a Different Content of a Polymer Binder in a High-Enthalpy Gas Flow. pp. 61--66

V.L. Strakhov, A.A. Filipenko, A.V. Ostrik, A.B. Mitkevich, Vl.O. Kaledin, M.N. Slitkov
Complex Model of Interaction of Composites with Radiation and a Gas Flow. pp. 67--74

A.K. Alekseev, M.P. Shuvalov
Thermal Protection Based on Crystalline Hydrates. pp. 75--79

E.M. Ovsyannikov
Use of Solar Furnaces under Orbital-Flight Conditions. pp. 80--85

S.A. Shargarovskii, A.N. Temnov
Trajectories of an Unguided Probe with a Damping Cable. pp. 86--89

V.S. Khokhulin
Algorithmic and Program Software for Combinatorial Simulation of the Thermal Regime of Space Objects. pp. 90--100

V.M. Yudin
Combined Method for Calculating Temperature Fields in the Structure of Aircraft. pp. 101--106

V.N. Eliseev
Calculation of Radiative-Conductive Heat Transfer in a System Closed by a Semitransparent Envelope. pp. 107--112

V.A. Burakov, E.N. Korchagin, V.P. Kozhukhov, A.S. Tkachenko, I.V. Schcherbakov
Mathematical Simulation of Heat Exchange in a Nonhermetic Instrumental Compartment of a Spacecraft. pp. 113--124

A.V. Attetkov, I.K. Volkov
Analytical Methods of Investigation of the Thermal State of a Region with a Moving Boundary under the Conditions of Nonstationary Heat Transfer to the External Medium. pp. 125--130

B.B. Petrikevich, S.D. Panin, A. V. Astrakhov
Use of Integral Boundary-Layer Theory for Solving Conjugate Problems of Heat Transfer in Channels of High-Power Plants. pp. 131--137

V.S. Zarubin, G.N. Kuvyrkin
Mathematical Modeling of Thermomechanical Processes in Aircraft Structures. pp. 138--144

N.N. Golovin, G.N. Kuvyrkin
Problems of Numerical Modeling of the Temperature and Stress Fields in the Structures of SFRE Nozzle Blocks. pp. 145--154

A.Yu. Bushuev, V.V. Gorskii
Selectivity Functions and a Two-Contour Algorithm as a Tool Used in the Problems of Synthesis of Multilayer Constructions. pp. 155--159

V.I. Kuznetsov, D.D. Shpakovskii
Anomalous Aerodynamic Heating of a Dead-End Cavity in an Oncoming Flow. pp. 160--164

V.V. Orlov, A. N. Temnov
Oscillations of a Rotary Fluid Flowing out of a Closed Vessel. pp. 165--173

S.T. Surzhikov
Nonstationary Radiation-Gasdynamic Model of a Laser-Plasma Accelerator. pp. 174--179

E.V. Borisov, O.G. Martynov, V.N. Mironov, E.F. Nogotov
Interaction of Shock and Detonation Waves in Gas Media with Dispersed Materials and Solid Barriers. pp. 180--188

A.V. Kotovich, G.A. Nesenenko
Allowance for Mutual Effect of "Hot Spots" in Solution of Problems of Site Thermal Explosion. pp. 189--192

A.V. Kotovich, G.A. Nesenenko
Parametric Analysis of Site Modes of Thermal Explosions by a "Geometrical-Optical" Asymptotic Method. pp. 193--197

A.V. Kostanovskii, L.A. Zhilyakov
Conditions for Producting the Liquid Phase of Carbon. pp.198--201

V.F. Mitin, N.S. Boltovets, V.V. Kholevchuk, R.V. Konakova
Germanium-Film Resistance Microthermometers Intended for Operation within the Temperature Range of 0.03-300 K. pp. 202--205

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