Air Density Calculator
Calculate air density from pressure, temperature, and humidity using the ideal gas law. Includes altitude reference table and moist air corrections.
Calculate first cell height for CFD mesh y⁺ requirements. Includes Reynolds number, friction velocity, boundary layer region guide, and y⁺ reference table.
| y⁺ | Wall Distance | Region |
|---|---|---|
| 0.1 | 0.8 µm | Viscous sublayer |
| 0.5 | 3.9 µm | Viscous sublayer |
| 1 | 7.7 µm | Viscous sublayer |
| 2 | 15.4 µm | Viscous sublayer |
| 5 | 38.6 µm | Buffer layer |
| 10 | 77.2 µm | Buffer layer |
| 30 | 0.232 mm | Log-law region |
| 50 | 0.386 mm | Log-law region |
| 100 | 0.772 mm | Log-law region |
| 200 | 1.544 mm | Log-law region |
| 300 | 2.317 mm | Outer layer |
Y-plus (y⁺) is a dimensionless wall distance used in computational fluid dynamics (CFD) to determine whether your near-wall mesh resolution is adequate for the chosen turbulence model. It's defined as y⁺ = yρu*/µ, where y is the distance from the wall, ρ is density, u* is the friction velocity, and µ is dynamic viscosity. Getting y⁺ right is arguably the most important step in CFD mesh generation.
Different turbulence models require different y⁺ ranges. Low-Reynolds-number models like k-ω SST need y⁺ ≈ 1 at the wall — the first cell must be entirely within the viscous sublayer. Wall-function models (standard k-ε) need y⁺ = 30-300 — the first cell should be in the log-law region. Using the wrong y⁺ range for your turbulence model produces incorrect wall shear stress, heat transfer, and separation predictions.
This calculator estimates the first cell height needed to achieve a target y⁺ using the flat-plate skin friction correlation. It also provides reverse calculation (y⁺ from given cell height), fluid property presets, and a full y⁺ range table showing which boundary layer region each value falls in.
Every CFD engineer checks y⁺ before meshing because the wrong first cell height either wastes computation or gives the wrong wall treatment. This calculator replaces manual spreadsheets and gives a fast first estimate for air, water, and other common flows, so you can set a wall-distance target before you build the prism layers.
y = y⁺µ/(ρu*). Friction velocity: u* = √(τw/ρ). Wall shear: τw = ½CfρU². Skin friction (Schlichting): Cf = 0.058Re⁻⁰·². Reynolds number: Re = ρUL/µ.Result: First cell: 0.0078 mm, Re = 3.4M, u* = 1.87 m/s
Air at 50 m/s over a 1 m plate: Re = 3.4M (turbulent). Cf = 0.058 × (3.4e6)^-0.2 = 0.0028. τw = 0.5 × 0.0028 × 1.225 × 50² = 4.3 Pa. u* = √(4.3 / 1.225) = 1.87 m/s. y = 1 × 1.789e-5 / (1.225 × 1.87) = 7.8 µm = 0.0078 mm.
Use y⁺ to decide whether the first cell sits in the viscous sublayer or in the wall-function region. That interpretation matters more than the number itself, because the same y⁺ target can imply very different physical cell heights in air, water, or high-speed flow.
The flat-plate estimate is a starting point, not a final mesh rule. Real geometries need local checks after the solver runs, especially around separation points, curvature, and changing Reynolds number.
If you are using k-ω SST, aim for y⁺ near 1. If you are using a wall-function approach, aim for the range your model expects and keep layer growth smooth enough that the near-wall grid does not collapse.
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A dimensionless wall distance: y⁺ = yρu*/µ. It locates. the first mesh cell within the boundary layer structure: y⁺ < 5 is the viscous sublayer, 5-30 is the buffer layer, 30-300 is the log-law region.
Low-Re models resolve the viscous sublayer (need y⁺ ≈ 1). Wall-function models bridge the sublayer with empirical laws (need y⁺ = 30-300). Wrong y⁺ → wrong physics.
u* = √(τw/ρ) — a velocity scale derived from wall shear stress. It characterizes the turbulent boundary layer near the wall and is the key to the y⁺ definition.
Enough to span the boundary layer (~10-30 layers). With growth ratio 1.2 and first cell at y⁺=1, 15-20 layers typically cover the boundary layer for external flows.
This is normal — y⁺ varies with local velocity and geometry. Aim for average y⁺ in range, and accept some variation. Separation regions will have lower y⁺ than attached flow.
Yes — use pipe diameter as reference length and bulk velocity as U. The flat-plate analogy gives a reasonable initial estimate; check y⁺ after solving.
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