Limits of Fluid Modeling for High Pressure Flow Simulations
Flows in liquid propellant rocket engines (LRE) are characterized by high pressures and extreme temperature ranges, resulting in complex fluid behavior that requires elaborate thermo-physical models. In particular, cubic equations of state and dedicated models for transport properties are firmly est...
Main Authors: | Nelson P. Longmire, Daniel T. Banuti |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-10-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/9/11/643 |
Similar Items
-
Analysis of heat transfer mechanism in supercritical fluids from the aspect of pool heating
by: Minyun Liu, et al.
Published: (2023-01-01) -
Numerical Investigation of Heat Transfer Characteristics of scCO<sub>2</sub> Flowing in a Vertically-Upward Tube with High Mass Flux
by: Kaigang Gong, et al.
Published: (2022-01-01) -
Particle formation with supercritical fluids : challenges and limitations /
by: editor
Published: (2014) -
Overview of Common Thermophysical Property Modelling Approaches for Cryogenic Fluid Simulations at Supercritical Conditions
by: Jaya Vignesh Madana Gopal, et al.
Published: (2023-01-01) -
A study of boiling water flow regimes at low pressures
by: Fiori, Mario P., et al.
Published: (2011)