Uprating the Frontal Thrust of a Spherical Gas-Dynamical Resonator-Pulse Amplifier
Calculations were carried out with application of current numerical methods and with the use of scientific-technical developments of a gas-dynamical resonator-thrust amplifier. The possibility of creating an exit device with a resonator for a small-size gas-turbine engine that in flight provides for...
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Published in | Journal of engineering physics and thermophysics Vol. 90; no. 1; pp. 176 - 180 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
New York
Springer US
2017
Springer |
Subjects | |
Online Access | Get full text |
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Summary: | Calculations were carried out with application of current numerical methods and with the use of scientific-technical developments of a gas-dynamical resonator-thrust amplifier. The possibility of creating an exit device with a resonator for a small-size gas-turbine engine that in flight provides for thrust uprating by no less than 6% via gas mass attachment in the pulsating process is shown. In this way the size–mass characteristics of the exit device are preserved in the process. |
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Bibliography: | ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
ISSN: | 1062-0125 1573-871X |
DOI: | 10.1007/s10891-017-1553-6 |