IndisputableMonolith.Flight.Pressure
The Flight.Pressure module converts a logarithmic vorticity proxy into a positive magnitude proxy for pressure calculations inside the discrete flight medium scaffold. Researchers modeling φ-vortex propulsion would cite it when bridging vorticity to pressure observables. The module consists entirely of definitions and algebraic proxies imported from Medium and ILG.PressureForm.
claimGiven log-vorticity proxy satisfying logVorticity ≈ log |ω|, define ω_mag ≈ |ω|. Introduce PressureParams and the pressure proxy p := ρ · w(k,a) · δ together with PressureDropFromVorticity and the equivalence pressure_eq_proxy.
background
The module sits inside the discrete scaffold of Flight.Medium, which supplies a minimal medium-state interface built on a vorticity proxy and is intentionally decoupled from LNAL. It imports the algebraic display equivalence from ILG.PressureForm that rewrites the ILG effective source term as the pressure variable p := ρ · w(k,a) · δ while keeping the underlying physics unchanged. The module then supplies the conversion omegaMag together with PressureParams, pressureProxy, PressureDropFromVorticity and pressure_eq_proxy.
proof idea
This is a definition module, no proofs. It structures the content by declaring the magnitude conversion omegaMag from the imported log-vorticity proxy, followed by the pressure-parameter record and the proxy definitions that rest directly on the Medium and PressureForm interfaces.
why it matters in Recognition Science
The module feeds the IndisputableMonolith.Flight facade, whose purpose is to re-export submodules while keeping lemmas provable in Lean and isolating physical hypotheses, and the Flight.Thrust layer that defines a minimal thrust-observable interface. It supplies the pressure-proxy step required by the spiral-field propulsion scaffold for φ-Vortex Drive.
scope and limits
- Does not claim a continuum Navier-Stokes model.
- Does not derive surface integrals or control-volume statements.
- Does not connect directly to the LNAL framework.
- Does not include numerical validation or empirical checks.
- Does not supply full thrust-vector derivations.