Compute the stagnation (total) pressure from static pressure and flow speed using p₀ = p + ½ρv², for Pitot-based velocity measurement, inlet design and wind tunnel pressure conversion.
| Item | Formula / Note | Source / Standard |
|---|---|---|
| Stagnation pressure | p₀ = p + ½ρv², incompressible | Bernoulli's equation, 1738 |
| Compressible correction | Isentropic stagnation ratio | Anderson, Aerodynamics |