230 likes | 363 Vues
This study investigates the turbulent fluctuations in the intake process at varying conditions, specifically at different crank angles (CA) ranging from 292 to 314 degrees. We analyze static pressure, Mach number, temperature, and kinetic energy across multiple hydraulic values (hv) ranging from 0 to 4 mm. The data sets provide insight into the aerodynamic performance and flow characteristics, essential for optimizing intake systems in engineering applications, particularly in combustion and jet propulsion.
E N D
hv = 0 mm Process of intake CA=292 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 0.14 mm Process of intake CA=293 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 0.78 mm Process of intake CA=294 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 1.7 mm Process of intake CA=295 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 2.66 mm Process of intake CA=296 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 3.47 mm Process of intake CA=297 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 3.9 mm Process of intake CA=298 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=299 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=300 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=301 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=302 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=303 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=304 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=305 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 4 mm Process of intake CA=306 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 3.9 mm Process of intake CA=307 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 3.47 mm Process of intake CA=308 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 2.66 mm Process of intake CA=309 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 1.7 mm Process of intake CA=310 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 0.78 mm Process of intake CA=311 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 0.14 mm Process of intake CA=312 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 0 mm Process of intake CA=313 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations
hv = 0 mm Process of intake CA=314 deg Static Pressure Mach Number Temperature Kinetic Energy of Turbulent Fluctuations