Accuracy Setup
δρcyl
%, incylinder density
δρres
%, reciever density
δρexh
%, exhaust manifold density
δρint.res
%, intermidiate reciever density
δρint.exh
%, intermidiate exhaust manifold density
δΠk
%, pressure insrease ratio
δPTC
%, turbocharger's power balance
δΠk1
%, first-stage pressure insrease ratio
δΠk2
%, second-stage pressure insrease ratio
MeshGenerator Setup
Δφbase
CAD, basic mech step
Δφoverlap
CAD, mesh step for valves(ports) overlap
Δφcomb
CAD, mesh step for combustion
φcomb.mesh
CAD, duration of mesh segmentation for combustion
Core Setup
Nit
the limit for iterations
Nit.tra
the limit for transient iterations
Solution
the numeric method of solution
Use real gases state equations
Configure solutions options
Choose the supercharging system configuration
Choose the type of solution
Adjust to maximum pressure limit & maximum pressure rate limit
Use control maps to set combustion dynamically
Use equations to find pressure losses dynamically
Use advanced TMAP treatment
Compute Log
Error occured!
| Step | δρcyl, % | δρres, % | δρexh, % | δΠk, % | δPTC, % | δPb, % |
|---|
Advanced Compute Log
Error occured!
| Step | ρcyl, kg/m3 | ρres, kg/m3 | ρexh, kg/m3 | Πk | nTC, rpm | Pb, kW |
|---|
Transient Log
Error occured!
| It | τ, s | ncrank, rpm | Pb, kW | Pload, kW | α |
|---|
