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Khmelevskiĭ Alexander Nikolaevich

Publications in Math-Net.Ru

  1. Spectra signals of gas pressure pulsations in annular and linear dual slotted nozzles

    Combustion Science and Technology, 191:2 (2019),  339–352
  2. Investigation of the spectral composition of the gas pressure and thrust pulsations in nozzles equipped with a deflector

    Izv. Ross. Akad. Nauk Mekh. Zhidk. Gaza, 2019, no. 3,  123–137
  3. About Spectral Structure Management of Gas Pressure Pulsations Signals in Nozzles with Deflector

    Dokl. Akad. Nauk, 483:5 (2018),  506–509
  4. High Temperature Inflammation and Combustion of Methane

    BULLETIN of the L.N. Gumilyov Eurasian National University. MATHEMATICS.COMPUTER SCIENCE. MECHANICS Series, 125:4 (2018),  120–124
  5. Investigation of the annular nozzle start in actual and virtual intermittent aerodynamic setups

    Izv. Ross. Akad. Nauk Mekh. Zhidk. Gaza, 2016, no. 2,  158–165
  6. Unsteady laminar gas flows in an annular nozzle

    TVT, 54:6 (2016),  889–893
  7. Pulsating gas flows in an annular nozzle

    Dokl. Akad. Nauk, 465:1 (2015),  42–45
  8. Investigating an annular nozzle on combustion products of hydrocarbon fuels

    Теплофизика и аэромеханика, 20:3 (2013),  269–276
  9. Experimental and numerical simulation of the flow in a driving module with an annular and linear double-slot nozzle

    TVT, 51:5 (2013),  755–763
  10. Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle

    Fizika Goreniya i Vzryva, 48:4 (2012),  38–50
  11. Modeling of equilibrium combustion of kerosene by a mixture of gaseous hydrocarbons

    Fizika Goreniya i Vzryva, 43:4 (2007),  3–7
  12. Simulation of nitric oxide formation in combustion of methane-air mixtures

    Fizika Goreniya i Vzryva, 33:1 (1997),  12–23
  13. Features of combustion product flow structure in a spherical semi-open cavity

    Fizika Goreniya i Vzryva, 31:1 (1995),  32–40
  14. Formation of a nonequilibrium energy distribution over vibrational degrees of freedom of the H$_2$O molecule as water vapor expands in a supersonic nozzle

    Prikl. Mekh. Tekh. Fiz., 33:4 (1992),  32–42
  15. Characteristics of flow of water vapor with heating by shock waves and cooling in supersonic nozzles

    TVT, 30:4 (1992),  745–752
  16. Investigation of the flow inversion properties behind a block of small axisymmetric nozzles of a homogeneous gas-dynamic laser

    Fizika Goreniya i Vzryva, 27:5 (1991),  94–101
  17. Measurement of molecular constants of the vibrational-rotational transition $001(6_{33})\to020(5_{50})$ in water vapour behind the shock wave

    Dokl. Akad. Nauk SSSR, 309:1 (1989),  82–85
  18. Investigation of the effect of gasdynamic perturbations behind a deformed nozzle cluster on the inversion and power of a combustion CO$_2$ gasdynamic laser

    Fizika Goreniya i Vzryva, 25:6 (1989),  81–87
  19. Effect of outflow conditions on the characteristics of N$_2$O-GDL

    Fizika Goreniya i Vzryva, 24:1 (1988),  61–65
  20. Effects of ignition on gain in an inverted N$_2$O flow

    Fizika Goreniya i Vzryva, 23:3 (1987),  16–21
  21. ON THE ROLE OF IGNITION IN NOZZLE INJECTION IN N2O+N2+HE AND N2O+CO+HE GAS-DYNAMIC LASERS

    Zhurnal Tekhnicheskoi Fiziki, 57:5 (1987),  883–890
  22. Selection of a calculation model for nozzle flow in high-temperature combustionproduct gasdynamic lasers

    Kvantovaya Elektronika, 13:1 (1986),  86–94
  23. Modeling of flows of the products of combustion of hydrocarbon fuels in an impulsive setup of the explosive type

    Fizika Goreniya i Vzryva, 21:6 (1985),  34–41
  24. Investigation of the characteristics of an explosion-type gasdynamic laser utilizing the combustion products of acetylene

    Kvantovaya Elektronika, 8:5 (1981),  1002–1011


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