⚙️ 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)
1.416 kgs/kgm
Volumetric Ratio Rv = 49.558 m³s/m³m
Pressure Lift Ratio (N)
0.0380
ΔPlift = 0.30 bar | ΔPmot = 7.90 bar
Motive Jet Velocity (Vm)
564.28 m/s
ṁm = 2.680e-1 kg/s (229.75 m³/h)
Suction Entrained Flow (ṁs)
3.795e-1 kg/s
Qs = 11385.83 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 : Steam Jet Vacuum Ejector (Condenser Exhaust) Motive Pressure (Pm) : 8.00 bar abs (8.000e+5 Pa) Suction Pressure (Ps) : 0.10 bar abs (1.000e+4 Pa) Discharge Pressure (Pout) : 0.40 bar abs (4.000e+4 Pa) ----------------------------------------------------------------- Motive Nozzle Diameter : 12.00 mm Mixing Chamber Diameter : 45.00 mm Area Ratio (Am/Amix) : 0.0711 ----------------------------------------------------------------- Motive Jet Velocity (Vm) : 564.28 m/s Motive Mass Flow (mdot_m) : 2.6804e-1 kg/s (229.75 m3/h) Suction Mass Flow (mdot_s) : 3.7953e-1 kg/s (11385.83 m3/h) Total Discharge Flow : 6.4756e-1 kg/s (11615.57 m3/h) ----------------------------------------------------------------- Entrainment Mass Ratio Rm : 1.4160 kg_suction / kg_motive Volumetric Ratio Rv : 49.5585 m3_suction / m3_motive Pressure Lift Ratio N : 0.03797 Hydraulic Efficiency : 0.65 % Mixing Velocity (V_mix) : 2028.72 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 $\eta_{diff} \approx 0.75 - 0.85$.