2020
DOI: 10.1016/j.ast.2020.105786
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Effect of fuel-jet injection angle variation on the overall performance of a SCRAMJET engine

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Cited by 40 publications
(4 citation statements)
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“…(1991 a ), Fuller, Thomas & Schetz (1991 b ), Aso et al. (2009), Sharma, Eswaran & Chakraborty (2020) and Sebastian, Lürkens & Schreyer (2020).…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…(1991 a ), Fuller, Thomas & Schetz (1991 b ), Aso et al. (2009), Sharma, Eswaran & Chakraborty (2020) and Sebastian, Lürkens & Schreyer (2020).…”
Section: Introductionmentioning
confidence: 99%
“…Single jets injected at a spanwise or streamwise inclination have been studied by e.g. Fuller et al (1991a), Fuller, Thomas & Schetz (1991b), Aso et al (2009), Sharma, Eswaran & Chakraborty (2020) and Sebastian, Lürkens & Schreyer (2020).…”
Section: Introductionmentioning
confidence: 99%
“…The advances in the image processing methodologies and camera sensors allow the measurement of the smallest particles present in a spray with high accuracy. There are experimental and numerical studies applied to different ambient conditions and regimes of cross flow, specially focused in atomization of the spray and liquid jet breakup [1][2][3][4][5]. In those studies the optical techniques were the cornerstone for the data acquisition and validation of the simulations.…”
Section: Introductionmentioning
confidence: 99%
“…Also recent studies from Huh and Lee [21], Zhao et al [22], Williams et al [30], Liu et al [24] numerically investigated the interaction of the jets with supersonic cross flow using high fidelity numerical methods. In addition various authors examined jets in supersonic cross flow in a scramjet engine, numerically [27], [28], [29], [30]. Specifically Miller et al [25] numerically investigated transient interaction between a reaction control jet and Mach 5 cross flow using data from the thesis of Erdem [26].…”
Section: Introductionmentioning
confidence: 99%