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Correction of low-Reynolds number turbulence model to hydrocarbon fuel at supercritical pressure
- Source :
- Aerospace Science and Technology. 77:156-167
- Publication Year :
- 2018
- Publisher :
- Elsevier BV, 2018.
-
Abstract
- At supercritical pressure, due to the drastic change of thermophysical property near the pseudo-critical temperature, the density fluctuation and density variation, along with buoyancy, play an important role in supercritical turbulence modelling. Based on the original LS (Launder–Sharma) low-Reynolds number turbulence model, the buoyancy modification, the density fluctuation modification, the density variation modification and the empirical coefficients modification are considered and the corresponding correction terms are derived and applied in the governing equations. Numerical simulation of heat transfer to hydrocarbon fuel flowing through the uniformly heated round pipe at supercritical pressure has been performed by the modified LS turbulence model incorporated into the in-house numerical code. Inlet temperature varied from 373 K to 473 K, with heat flux varying from 241 kW/m2 to 470 kW/m2. Inlet mass flux was 736 kg/(m2⋅s) and operating pressure was 4 MPa. The flow directions included upflow and downflow. Compared with the original LS turbulence model, the modified LS turbulence model leads to the better agreement with the experimental results, with 41.16% improvement in computation accuracy in the current study. The consideration of density fluctuation and density variation effects makes the turbulence model more suitable for thermophysical property variation at supercritical pressure.
- Subjects :
- Mass flux
Buoyancy
Materials science
Turbulence
Flow (psychology)
Aerospace Engineering
Reynolds number
02 engineering and technology
Mechanics
engineering.material
01 natural sciences
Supercritical fluid
010305 fluids & plasmas
Physics::Fluid Dynamics
symbols.namesake
020303 mechanical engineering & transports
0203 mechanical engineering
Heat flux
0103 physical sciences
Heat transfer
symbols
engineering
Subjects
Details
- ISSN :
- 12709638
- Volume :
- 77
- Database :
- OpenAIRE
- Journal :
- Aerospace Science and Technology
- Accession number :
- edsair.doi...........8a49c7da29fcf0ab0e5b2b5d5848a657