Results 11 to 20 of about 39,762 (260)
Beneficial Effects of Guide Fins on Corner Separation
Volume 13A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, 2023 Abstract Corner separation is a major phenomenon limiting the operability of aeronautical compressors. Passive control devices such as guide fins are envisioned to reduce its deleterious effects. In this paper, guide fins are optimized to reduce the total pressure losses downstream of a subsonic compressor cascade (M = 0.11, Re = 3.2 105,
Mondin, Gabriel +3 more
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Influence of expansion corner on the interaction of dual separation zones
AIP Advances, 2022 The complex shock waves/boundary layer interaction is an important problem in inlets, which induces the interaction of multiple separation zones and has attracted experts’ attention gradually.
Zi-yuan Zhu +4 more
doaj +1 more source
Once again on the supersonic flow separation near a corner [PDF]
Journal of Fluid Mechanics, 2002 Laminar boundary-layer separation in the supersonic flow past a corner point on a rigid body contour, also termed the compression ramp, is considered based on the viscous–inviscid interaction concept. The ‘triple-deck model’ is used to describe the interaction process.
Korolev, G. L. +2 more
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Optimization of Sweep and Blade Lean for Diffuser to Suppress Hub Corner Vortex in Multistage Pump
Machines, 2021 The bowl diffuser is the main flow component in multistage submersible pumps; however, secondary flow fields can easily induce a separation vortex in the hub corner region of the bowl diffuser during normal operation. To explore the flow mechanism of the
Chao Ning, Puyu Cao, Xuran Gong, Rui Zhu
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Influence of Ellipsoidal Dimple Column Number on Performance of Highly-loaded Compressor Cascade [PDF]
Journal of Applied Fluid Mechanics, 2023 The impact of the column number of ellipsoidal dimples on a highly-loaded compressor cascade (NACA65-K48) under design conditions was investigated by using a numerical simulation method.
H. W. Lu +4 more
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Toward the Utilization of 3D Blading in the Cantilevered Stator from Highly Loaded Compressors
Applied Sciences, 2023 Three-dimensional blading is an efficient technique in compressor aerodynamic design, and its function mechanism in the cantilevered stator needs to be addressed. This paper focuses on the sweep and dihedral in the cantilevered stator and seeks to expose
Xiaobin Xu +5 more
doaj +1 more source
Global Visualization of Compressible Swept Convex-Corner Flow Using Pressure-Sensitive Paint
Aerospace, 2021 This study used pressure-sensitive paint (PSP) and determined the surface pressure distributions for a compressible swept convex-corner flow. The freestream Mach numbers were 0.64 and 0.83.
Kung-Ming Chung, Yi-Xuan Huang
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Tiirbuient Boundary Layer Flow over S-Shaped Surface With Side W Parallel to the Stream [PDF]
The Egyptian International Journal of Engineering Sciences and Technology, 2000 TurhukiU boimdarv layers over s-shaped surface atlacbed to a verfical side wall wereExperimeufally mvesfigafed. Measurements were performed over the s-shaped surfaceAt three distinctive regions; the neighborhood of the corner; a distance ...
ma Hlawa
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Turbulence modelling analysis in a corner separation flow [PDF]
Computers & Fluids, 2020 zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Monier, Jean-François +3 more
openaire +1 more source
Engineering Applications of Computational Fluid Mechanics, 2022 Air injection is an effective method to eliminate flow separation and improve blade loading in compressors. In existing studies on unsteady air injection, achieving a better control effect than steady injection with lower injection consumption is a major
Zhiyuan Cao +5 more
doaj +1 more source