Journal of Fluid Mechanics· 2026Q1
An analytical model for rotors in confined flow across operating regimes
- 0citations
- Q1SCImago
- 2026year
Short summary
A new Unified Blockage Model (UBM) accurately predicts rotor performance in confined flows across a wide range of thrust coefficients and misalignment angles, outperforming existing models limited to low thrust.
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Key points
- Developed the Unified Blockage Model (UBM) for rotors in confined flows, applicable at arbitrary thrust coefficients and misalignment angles.
- The UBM shows excellent agreement with large eddy simulations, capturing coupled interactions between thrust, misalignment, and blockage.
- Incorporated UBM into a blade-element momentum model and validated against blade-resolved simulations across various tip-speed and blockage ratios.
- Developed and validated a blockage correction method based on the UBM against numerical and experimental data.
AI-generated from the title and abstract; the full text is not read.
Abstract
Rotors operating in confined flows, or blockage, are commonly encountered in wind and water tunnels, as well as in shallow or dense deployments of hydrokinetic turbines. Confinement induces a streamwise pressure gradient in the channel, modifying the rotor induction, thrust and power. To account for these effects, physics-based or empirical blockage corrections are used as a transfer function between the dynamics of an object operating in confined and unconfined settings. However, existing blockage models are largely only applicable to rotors operating at relatively low thrust coefficients, such that the assumptions of classical momentum theory are valid. Further, rotors are often partially misaligned with the inflow, which modifies both the geometric blockage and the thrust force, whereas existing blockage models assume perfectly aligned flow conditions. We develop a generalised engineering model for an actuator disk operating in confined flow at arbitrary misalignment angles and thrust coefficients, termed the Unified Blockage Model (UBM). The analytical model shows excellent agreement with large eddy simulations of an actuator disk and elucidates the coupled interactions between thrust, misalignment and blockage. To predict bladed rotor dynamics, the UBM is incorporated into a blade-element momentum model framework and validated against blade-resolved simulations across a wide range of tip-speed and blockage ratios. Finally, a blockage correction method is developed based on the UBM and validated against a suite of numerical and experimental data.
The authors' abstract, as published at the source. Journal of Fluid Mechanics, 2026 · DOI ↗
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Field: Aerospace Engineering
Aerospace EngineeringEngineering