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TVT, 2013, Volume 51, Issue 5, Pages 755–763 (Mi tvt138)  

This article is cited in 5 scientific papers (total in 5 papers)

Heat and Mass Transfer and Physical Gasdynamics

Experimental and numerical simulation of the flow in a driving module with an annular and linear double-slot nozzle

V. A. Levinab, N. E. Afoninaab, V. G. Gromovab, I. S. Manuilovichab, V. V. Markovab, G. D. Smekhovab, A. N. Khmelevskiiab

a Steklov Institute of Mathematics, Moscow, Russia
b Scientific Research Institute of Mechanics, Moscow State University, Moscow, Russia

Abstract: This paper presents the results of numerical and experimental studies of the flow and comparison of propulsion performance characteristics of a model of a jet engine exhaust system equipped with an annular or (equivalent in gas consumption) linear double-slot nozzle with an inner cavity and circular segment deflector in the axial section. Calculations performed for the annular nozzle and double-slot nozzle corresponding to it in geometric parameters demonstrate that a flow similar to the flow in nozzles with a central body is formed in the exhaust system. According to the data obtained, the initial turn of the flow takes place in the oblique shock wave. In the double-slot nozzle, the final turn of the flow in the direction of the thrust vector occurs in a configuration of four shock waves positioned downwards in the flow; in the annular nozzle, it is in the intense barrel shock wave. It was established that the exhaust system with an annular of the linear doubleslot nozzle develops a thrust and specific impulse that exceed the corresponding values for the sonic nozzle equivalent in gas consumption by almost a factor of 2.

Funding Agency Grant Number
Russian Foundation for Basic Research 11-01-00068-а
12-01-90416-Укр_а
Ministry of Education and Science of the Russian Federation НШ-5911.2012.1
МК-3355.2012.1
Russian Academy of Sciences - Federal Agency for Scientific Organizations


DOI: https://doi.org/10.7868/S0040364413050141

Full text: PDF file (825 kB)
References: PDF file   HTML file

English version:
High Temperature, 2013, 51:5, 681–689

Bibliographic databases:

UDC: 533.697+544.452+519.63
Received: 26.07.2012

Citation: V. A. Levin, N. E. Afonina, V. G. Gromov, I. S. Manuilovich, V. V. Markov, G. D. Smekhov, A. N. Khmelevskii, “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; High Temperature, 51:5 (2013), 681–689

Citation in format AMSBIB
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\by V.~A.~Levin, N.~E.~Afonina, V.~G.~Gromov, I.~S.~Manuilovich, V.~V.~Markov, G.~D.~Smekhov, A.~N.~Khmelevskii
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\jour TVT
\yr 2013
\vol 51
\issue 5
\pages 755--763
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\crossref{https://doi.org/10.7868/S0040364413050141}
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\jour High Temperature
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\vol 51
\issue 5
\pages 681--689
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    Citing articles on Google Scholar: Russian citations, English citations
    Related articles on Google Scholar: Russian articles, English articles

    This publication is cited in the following articles:
    1. V. A. Levin, I. S. Manuylovich, V. V. Markov, “Numerical simulation of spinning detonation in circular section channels”, Comput. Math. Math. Phys., 56:6 (2016), 1102–1117  mathnet  crossref  crossref  mathscinet  zmath  isi  elib  elib
    2. V. A. Levin, N. E. Afonina, V. G. Gromov, I. S. Manuilovich, V. V. Markov, G. D. Smekhov, A. N. Khmelevskiǐ, “Unsteady laminar gas flows in an annular nozzle”, High Temperature, 54:6 (2016), 837–841  mathnet  crossref  crossref  mathscinet  isi  elib
    3. V. M. Abashev, I. N. Eremkin, N. P. Zhivotov, V. P. Zamuraev, A. P. Kalinina, P. K. Tret'tyakov, V A. Tupikin, “Experimental and computational modeling of the processes of supersonic outflow from a half-closed channel”, J. Eng. Phys. Thermophys., 91:2 (2018), 339–348  crossref  isi  scopus
    4. Afonina N.E. Gromov V.G. Levin V.A. Manuilovich I.S. Markov V.V. Khmelevskii A.N., “Investigation of the Spectral Composition of the Gas Pressure and Thrust Pulsations in Nozzles Equipped With a Deflector”, Fluid Dyn., 54:3 (2019), 414–427  crossref  isi  scopus
    5. Levin V.A. Afonina N.E. Gromov V.G. Manuylovich I.S. Khmelevsky A.N. Markov V.V., “Spectra Signals of Gas Pressure Pulsations in Annular and Linear Dual-Slotted Nozzles”, Combust. Sci. Technol., 191:2 (2019), 339–352  crossref  isi  scopus
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