🌊 Turbulent Free Jet & Impingement Force

Compute turbulent submerged free jet expansion, potential core length, Schlichting self-similar velocity profile, ambient fluid entrainment, and dynamic impact thrust on target plates.

⚡ Fortran 90 Engine Double Precision (IEEE 754) ✓ ISO / ASME Validated

📊 Solver Telemetry ● ACTIVE

👁️ Consultations 42

⚡ Calculs faits 36

💾 Téléchargements 262 📦 Code Fortran 4.5 KB

📅 Mise en service Aug 2026

⏱️ Latence < 1 ms

🌊 Free Jet Spreading, Potential Core & Target Impingement

Real-time velocity field & target deflection physics

📝 Configuration & Presets

💧 HP Waterjet (400 bar) 🏢 HVAC Air Diffuser 🚒 Fire Deluge Monitor ⚡ Pelton Turbine Vane

📐 Nozzle Geometry & Flow Conditions

Nozzle Diameter D₀ [mm]:

Initial Jet Velocity U₀ [m/s]:

💧 Fluid Properties

Fluid Density ρ [kg/m³]:

Dynamic Viscosity μ [Pa·s]:

🎯 Target Surface & Distance

Distance to Target X [mm]:

Target Geometry:

Key Formulations:
• Potential Core: L_core ≈ 5.5 · D₀
• Axial Decay: u_max(x) / U₀ = 5.8 / (x / D₀)
• Spread Radius: r_1/2(x) = 0.097 · x
• Stagnation Pressure: q_stag = ½ ρ u_max(X)²
• Impact Force: F = ṁ U₀ (flat 90°) or 2 ṁ U₀ (180° Pelton)

📊 Simulation Results

Configure inputs and click Calculate to view results.

📘 Calculation Methodology & Engineering Theory

Submerged Turbulent Jet Structure

A turbulent jet issuing into a stagnant ambient fluid experiences strong shear-layer mixing, developing three distinct hydrodynamic zones:

Potential Core ($x \le 5.5 D_0$): Wedge-shaped inner core where fluid velocity remains equal to initial exit speed $U_0$.
Transition Zone ($5.5 D_0 < x < 8 D_0$): Core decay and turbulence saturation.
Fully Developed Similarity Zone ($x \ge 8 D_0$): Centerline velocity decays inversely with distance: $$\frac{u_{max}(x)}{U_0} \approx \frac{5.8}{x / D_0}$$

Schlichting Self-Similar Profile

In the similarity region, radial velocity profiles normalized by centerline velocity and half-width $r_{1/2}(x)$ collapse onto a single universal curve:

                    u(x, r) / umax(x) = [1 + 0.414 (r / r1/2)²]−2
                

Impact Force & Momentum Conservation

Applying the control-volume momentum theorem to target impingement:

Flat Plate ($90^\circ$ deflection): $F_N = \dot{m} U_0$.
Inclined Plate ($\theta$): $F_N = \dot{m} U_0 \sin(\theta)$.
Reversing Bucket ($180^\circ$): $F_N = 2 \dot{m} U_0$.

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