Jet Conditions
While paused, move the sliders to update the result instantly.
$r_{1/2}/D \approx 0.1 \cdot x/D$
$U(r) = U_c \exp(-\ln 2 \cdot (r/r_{1/2})^2)$
$\Theta(r) \approx U(r)/U_c$ (Pr_t ≈ 0.7)
Simulate velocity and temperature profile development of free and impinging jets. Adjust exit velocity, nozzle diameter, and temperature excess to explore mixing layer growth and similarity laws.
While paused, move the sliders to update the result instantly.
The behavior of a turbulent free jet is governed by the conservation of momentum. For a circular jet, the centerline velocity decays inversely with distance from the nozzle.
$$ \frac{U_c}{U_0}= \frac{K}{\left(\frac{x}{D}\right)} $$Where $U_c$ is the centerline velocity at distance $x$, $U_0$ is the initial jet velocity, $D$ is the nozzle diameter, and $K$ is an empirical constant (typically around 6.3 for a circular jet). This shows the jet slows down as it entrains surrounding fluid.
The jet also grows linearly. The width of the jet (e.g., the half-width $b$, where velocity drops to half of $U_c$) increases proportionally to the distance.
$$ b = \beta x $$Here, $\beta$ is the spread rate, a key empirical constant that differs between jet types. For a circular jet, $\beta \approx 0.1$. This linear growth is why jets from a small nozzle can affect a large area far downstream.
HVAC System Design: Engineers use jet mixing analysis to place air diffusers and ensure uniform temperature without drafts. Calculating the throw (distance where velocity decays to 0.25 m/s) is essential for selecting the correct diffuser size and type for a room.
Industrial Burners and Combustion: The mixing rate of a fuel jet with air controls flame stability and efficiency. A poorly designed jet can lead to incomplete combustion, excess pollution, and hot spots that damage equipment.
Environmental Discharge: When wastewater or cooling water is discharged into a river or ocean, it forms a jet. Predicting its dilution rate is critical for environmental impact assessments to ensure pollutants are quickly mixed to safe concentrations.
Aerospace Engine Design: The mixing of high-speed exhaust jets with the ambient air affects thrust and noise. Engineers model these jets to optimize nozzle geometry for performance and to meet noise regulations near airports.
Model assumptions: The mathematical model used here relies on simplifying assumptions such as linearity, homogeneity, and isotropy. Always verify that your real system satisfies these assumptions before applying results directly to design decisions.
Units and scale: Many calculation errors arise from unit conversion mistakes or order-of-magnitude errors. Pay close attention to the units shown next to each parameter input.
Validating results: Always sanity-check simulator output against physical intuition or hand calculations. If a result seems unexpected, review your input parameters or verify with an independent method.
Structural & Mechanical Engineering: Solid mechanics, elasticity theory, and materials science form the foundation for many of the governing equations used here.
Fluid & Thermal Engineering: Fluid dynamics and heat transfer share similar mathematical structures (conservation equations, boundary-value problems) and frequently appear in multi-physics problems alongside structural analysis.
Control & Systems Engineering: Dynamic system analysis, state-space methods, and signal processing connect to the time-dependent behaviors modeled in this simulator.
For a confined impinging jet: uj=20 m/s, diam=8 mm, dtj=35 K, uinf=0 m/s. The simulator shows maximum centerline velocity of 20 m/s at nozzle exit, decaying to 4.2 m/s at 10 nozzle diameters (80 mm). Temperature excess drops from 35 K to 8.6 K over the same distance due to entrainment and mixing. Radial velocity profiles exhibit Gaussian distribution; peak heat transfer occurs within 3–5 diameters of impingement surface.