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Journal Articles

Hydraulic Circuit Design Rules to Remove the Dependence of the Injected Fuel Amount on Dwell Time in Multijet CR Systems

Mirko Baratta, Andrea Emilio Catania, Alessandro Ferrari
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Research Papers
J. Fluids Eng. December 2008, 130(12): 121104.
https://doi.org/10.1115/1.2969443
Published Online: October 27, 2008
...Mirko Baratta; Andrea Emilio Catania; Alessandro Ferrari In multijet common rail (CR) systems, the capability to manage multiple injections with full flexibility in the choice of the dwell time (DT) between consecutive solenoid current pulses is one of the most relevant design targets. Pressure...
View Article titled, Hydraulic Circuit <span class="search-highlight">Design</span> Rules to Remove the Dependence of the Injected Fuel Amount on Dwell Time in Multijet CR Systems
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Topics: Design, Ejectors, Fuels, Pipes, Pressure, Rails, Oscillations, Waves, Nozzles
Journal Articles

Numerical Study of Unsteady Flows in a Scroll Compressor

M. M. Cui
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Technical Papers
J. Fluids Eng. September 2006, 128(5): 947–955.
https://doi.org/10.1115/1.2243300
Published Online: February 21, 2006
.... This unsteadiness controls the mechanisms responsible for the behavior of the scroll compressor components and their interactions. The dynamic nature inherent in the scroll compressors affects the performance and reliability of the scroll compressors. To improve and optimize the scroll compressor design for better...
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Topics: Compressors, Flow (Dynamics), Pressure, Design, Unsteady flow, Shapes, Temperature
Journal Articles

Design of a Low-Turbulence, Low-Pressure Wind-Tunnel for Micro-Aerodynamics

Michael J. Martin, Kevin J. Scavazze, Iain D. Boyd, Luis P. Bernal
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Technical Papers
J. Fluids Eng. September 2006, 128(5): 1045–1052.
https://doi.org/10.1115/1.2236128
Published Online: February 13, 2006
...Michael J. Martin; Kevin J. Scavazze; Iain D. Boyd; Luis P. Bernal A novel wind-tunnel facility has been designed for measurement of lift and drag on micromachined airfoils. The tunnel is designed to operate with pressures ranging from 0.15 to 1.0 atmosphere, over a velocity range of 30 to 100 m...
View Article titled, <span class="search-highlight">Design</span> of a Low-Turbulence, Low-Pressure Wind-Tunnel for Micro-Aerodynamics
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Topics: Design, Flow (Dynamics), Turbulence, Wind tunnels, Tunnels, Computational fluid dynamics, Reynolds number, Pressure, Boundary layers, Aerodynamics