Abstract
For an aero turbo-shaft engine, rain water enters the intake protection device and the morphology of water droplets after hitting the wall will affect the internal flow of the compressor. In this paper, Sommerfeld number was used to determine the shape of water droplets after they hit the wall. The flow field and characteristics of the compressor with inlet particle separator under different water ingestion conditions were studied with considering the impact of water film and droplets splashing near the wall. The results show that the entry of water droplets deteriorates the internal flow field of the compression component, and the water film affects the flow state of the airflow near the wall. Compared to the effect of the splashing factor, the viscous resistance effect of water film near the wall on the airflow and boundary layer can cause a significant reduction in the characteristics and stability of the compressor.
Funding source: National Natural Science Foundation of China
Award Identifier / Grant number: Grant No. 52006042
Funding source: HeiLongJiang Postdoctoral Fund
Award Identifier / Grant number: Grant No. LBH-Z20126
Funding source: National Science and Technology Major Project
Award Identifier / Grant number: 2017-I-0009-0010
Funding source: China Scholarship Council
Award Identifier / Grant number: No. 202006685005
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Author contributions: All the authors have accepted responsibility for the entire content of this submitted manuscript and approved submission.
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Research funding: This paper is funded by National Natural Science Foundation of China (Grant No. 52006042); HeiLongJiang Postdoctoral Fund (Grant No. LBH-Z20126); National Science and Technology Major Project (2017-I-0009-0010) and China Scholarship Council (No. 202006685005).
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Conflict of interest statement: The authors declare no conflicts of interest regarding this article.
Nomenclature (SI units)
- K
-
Sommerfeld number
- We p
-
Weber number of the droplet
- Re p
-
Reynolds number of the droplet
- h
-
height of any point in the water film (mm)
- k s
-
height of sand roughness (mm)
- M l
-
liquid water mass flow (kg/s)
- R–R
-
Rosin–Rammler
- α
-
absolute angle (°)
- σ p
-
surface tension coefficient of water droplets (N/m)
- δ
-
water film thickness (mm)
- v δ
-
water film velocity (m/s)
- τ a
-
air flow shear force (N/m2)
- τ p
-
water droplet shear force (N/m2)
- μ
-
dynamic viscosity coefficient (Pa s)
- ρ
-
liquid water density (kg/m3)
- SM
-
surge margin
- π
-
total pressure ratio
References
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Articles in the same Issue
- Frontmatter
- Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel
- An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil
- Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity
- Installed performance seeking control based on supersonic variable inlet/engine coupling model
- Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation
- The aerodynamic performance degradation analysis of a small high bypass turbofan engine compression system with fan rotor blade leading edge erosion
- Flow structure comparison of film cooling versus hybrid cooling: a CFD study
- Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis
- Effect of free boundary on the performance of single expansion nozzle
- Optimization and numerical investigation of combined design of blade and endwall on rotor 67
- Numerical study on the effect of distortion of S-duct on flow field and performance of a full annulus transonic fan
- Research on a high-precision real-time improvement method for aero-engine component-level model
- Uncertainty quantification by probabilistic analysis of circular fins
- Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine
- Study on the water ingestion performance of compressor with inlet particle separator
- The role of volume effect on the transient behavior of a transonic compressor
- Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall
- Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion
- Active subspace-based performance analysis of supersonic through-flow fan rotor
- Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation
- Numerical investigation of tip clearance flow in a variable geometry turbine with non-uniform partial clearance