Transitional pressure drop in a cavitied microchannel
Creators
- 1. MIIT Key Laboratory of Multifunctional Lightweight Materials and Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People's Republic of China
- 2. State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People's Republic of China
- 3. School of Mechanical and Aeronautical Engineering, University of the Witwatersrand, Johannesburg 2000, South Africa
Description
Microchannels have become prevalent as an integrated part of microfluidic devices in biochemistry and electronics applications. In such devices, the small scale results in a characteristically low Reynolds number laminar flow. The small scale also results in an associated high flow resistance. A design concept has been developed that reduced the flow resistance by featuring geometrically modified microchannels with cavities. Compared to an unmodified microchannel, the modification reduces flow resistance at low Reynolds numbers but conversely leads to higher flow resistance at high Reynolds numbers: i.e., a reversal of flow resistance occurred. Thus far, plausible fluidic mechanisms underlying such reversal have remained largely unstipulated. Based upon detailed pressure and flow field measurements, we stipulate that flow progression from laminar flow slippage to rotational vortices in cavitied microchannels is the main mechanism causing the reversal. We further clarify that the earlier transition of initial laminar flow to turbulent flow is triggered by instabilities generated along shear layers, formed between the mainstream flow and rotational vortices in each cavity.
Additional details
Identifiers
- DOI
- 10.1103/PhysRevFluids.9.044201;
- Crossref Funder ID
- 10.13039/501100001809;
Publishing Information
- Journal Title
- Physical Review Fluids
- Journal Volume
- 9
- Journal Issue
- 4
- Journal Page Range
- 16 pgs.
- ISSN
- 2469-990X
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- Subject category
- S75: CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY; S42: ENGINEERING;
- Descriptors DEI
- COMPARATIVE EVALUATIONS; DESIGN; FLUIDS; HOT WIRE ANEMOMETERS; INSTABILITY; LAMINAR FLOW; LAYERS; MODIFICATIONS; PRESSURE DROP; REYNOLDS NUMBER; SHEAR; TURBULENT FLOW; VORTICES
- Descriptors DEC
- ANEMOMETERS; DIMENSIONLESS NUMBERS; EVALUATION; FLUID FLOW; MEASURING INSTRUMENTS
Optional Information
- Copyright
- ©2024 American Physical Society
- Contract/Grant/Project number
- 12032010
- Notes
- Contact Email: Corresponding author: tongbeum.kim@nuaa.edu.cn; Record automatically processed
- Funding organization
- National Natural Science Foundation of China