2022
DOI: 10.1007/s11630-022-1564-2
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Aerodynamic Performance Improvement of a Highly Loaded Compressor Airfoil with Coanda Jet Flap

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Cited by 8 publications
(2 citation statements)
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“…Jet Flap (a) GF (b) Jet flap Fig. 2 Schematic of Gurney and its virtual type (Feng et al [24]) et al [26] and Jian et al [27] have recently employed the JF on a compressor airfoil to increase the wall-attachment effect and mitigate the secondary flow losses. This approach eventually improves the aerodynamic performance of the compressors.…”
Section: Trailing Edge Airfoilmentioning
confidence: 99%
“…Jet Flap (a) GF (b) Jet flap Fig. 2 Schematic of Gurney and its virtual type (Feng et al [24]) et al [26] and Jian et al [27] have recently employed the JF on a compressor airfoil to increase the wall-attachment effect and mitigate the secondary flow losses. This approach eventually improves the aerodynamic performance of the compressors.…”
Section: Trailing Edge Airfoilmentioning
confidence: 99%
“…The concept of supercritical airfoil commonly used in large passenger aircraft flying at transonic speeds was proposed by NASA in the 1960s. After more than half a century of research, supercritical airfoil design technology continues to innovate, especially the rapid development of Computational fluid dynamics technology has created good conditions for fine design and performance tradeoffs of airfoils 4 .…”
Section: Introductionmentioning
confidence: 99%