2015
DOI: 10.2298/tsci120405114c
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Investigation on the pressure matching performance of the constant area supersonic-supersonic ejector

Abstract: The pressure matching performance of the constant area supersonic-supersonic ejector has been studied by varying the primary and secondary Mach numbers. The effect of the primary fluid injection configurations in ejector, namely peripheral and central, has been investigated as well. Schlieren pictures of flow structure in the former part of the mixing duct with different stagnation pressure ratio of the primary and secondary flows have been taken. Pressure ratios of the primary and secondary flows at the limit… Show more

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Cited by 4 publications
(2 citation statements)
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“…At present, in the practice of rocketry, the development of cruise missiles with hypersonic flight speeds is intensively developing [1][2][3][4][5][6][7][8]. Using of ramjet engines on solid propellants is one of the most promising directions for solving the problem of increasing the speed of flight of flying apparatus in the atmosphere [2,3].…”
Section: Introductionmentioning
confidence: 99%
“…At present, in the practice of rocketry, the development of cruise missiles with hypersonic flight speeds is intensively developing [1][2][3][4][5][6][7][8]. Using of ramjet engines on solid propellants is one of the most promising directions for solving the problem of increasing the speed of flight of flying apparatus in the atmosphere [2,3].…”
Section: Introductionmentioning
confidence: 99%
“…For optimization efforts on the mixing chamber geometry, it could be pointed to the research published by Palacz et al [12]. Some scholars paid attention to changing the pressure and temperature operating conditions of ejectors with axial-radial [14] or axial-axial [15] flows. Composition of the inlet streams, e.g.…”
Section: Introductionmentioning
confidence: 99%