⚙️ Ejector & Eductor Jet Pump
Model high-velocity motive jet entrainment, suction flow rate, 1D mixing chamber momentum balance, pressure lift ratio (N), entrainment mass ratio (Rm), and diffuser recovery.
⚡ Fortran 90 Engine
Double Precision (IEEE 754)
✓ ISO / ASME Validated
📊 Solver Telemetry
● ACTIVE
👁️ Consultations
27
⚡ Calculs faits
21
💾 Téléchargements
330
📦 Code Fortran
4.5 KB
📅 Mise en service
Aug 2026
⏱️ Latence
< 1 ms
⚙️ Ejector / Eductor Fluid Entrainment Dynamics
High-speed motive jet, suction entrainment & diffuser pressure recovery📝 Configuration & Presets
Key Formulations:
• Motive Jet: Vm = Cv √(2(Pm − Ps)/ρm)
• Entrainment Ratio: Rm = ṁs / ṁm
• Pressure Lift Ratio: N = (Pout − Ps) / (Pm − Ps)
• Area Ratio: RA = Anozzle / Amix = (dm / dmix)²
• Motive Jet: Vm = Cv √(2(Pm − Ps)/ρm)
• Entrainment Ratio: Rm = ṁs / ṁm
• Pressure Lift Ratio: N = (Pout − Ps) / (Pm − Ps)
• Area Ratio: RA = Anozzle / Amix = (dm / dmix)²
📊 Performance Results
📊 Output Summary
Entrainment Mass Ratio (Rm)
3.501 kgs/kgm
Volumetric Ratio Rv = 3.039 m³s/m³m
Pressure Lift Ratio (N)
0.0984
ΔPlift = 0.30 bar | ΔPmot = 3.05 bar
Motive Jet Velocity (Vm)
23.24 m/s
ṁm = 3.689e-1 kg/s (1.33 m³/h)
Suction Entrained Flow (ṁs)
1.292e+0 kg/s
Qs = 4.04 m³/h | Eff. η = 0.7%
📈 Entrainment Ratio Rm vs Motive Pressure Pm
📉 Characteristic Pump Curve: Pressure Lift N vs Rm
================================================================= THERMOFLUIDCALC — EJECTOR & EDUCTOR PERFORMANCE REPORT ================================================================= Case Title : Venturi Dosing & Chemical Mixing Eductor Motive Pressure (Pm) : 4.00 bar abs (4.000e+5 Pa) Suction Pressure (Ps) : 0.95 bar abs (9.500e+4 Pa) Discharge Pressure (Pout) : 1.25 bar abs (1.250e+5 Pa) ----------------------------------------------------------------- Motive Nozzle Diameter : 4.50 mm Mixing Chamber Diameter : 12.00 mm Area Ratio (Am/Amix) : 0.1406 ----------------------------------------------------------------- Motive Jet Velocity (Vm) : 23.24 m/s Motive Mass Flow (mdot_m) : 3.6887e-1 kg/s (1.33 m3/h) Suction Mass Flow (mdot_s) : 1.2915e+0 kg/s (4.04 m3/h) Total Discharge Flow : 1.6604e+0 kg/s (5.37 m3/h) ----------------------------------------------------------------- Entrainment Mass Ratio Rm : 3.5013 kg_suction / kg_motive Volumetric Ratio Rv : 3.0386 m3_suction / m3_motive Pressure Lift Ratio N : 0.09836 Hydraulic Efficiency : 0.65 % Mixing Velocity (V_mix) : 13.20 m/s =================================================================
📘 Calculation Methodology & Engineering Theory
1D Momentum Conservation
Ejectors transfer momentum from a high-velocity driving jet to a low-pressure secondary fluid within a constant-area mixing throat:
(P1 − P2) Amix = ṁtotal V2 − (ṁm Vm1 + ṁs Vs1) + Ffriction
Diffuser Pressure Recovery
The mixed fluid decelerates in the diverging section, converting dynamic pressure into static pressure rise:
Pout = P2 + ηdiff · ½ ρmix (Vmix² − Vout²)
Key Engineering Assumptions
- Complete mixing achieved within the mixing tube length ($L_{mix} \approx 6 \text{ to } 8 \cdot d_{mix}$).
- Subsonic flow in mixing section (incompressible liquid or moderate gas velocity).
- Nozzle discharge coefficient $C_v \approx 0.92 - 0.96$.
- Diffuser static pressure recovery efficiency $\eta_{diff} \approx 0.75 - 0.85$.