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instrument mechanism / verified-clean

Lift Coefficient / Lift Force Calculator mechanism

The inspectable method record for Lift Coefficient / Lift Force Calculator, kept separate from implementation and qualification.

Status: VERIFIED_CLEANLifecycle: verified-clean

Model scope

The lift-force equation is correct under standard steady-flow aerodynamic assumptions. Verdict is NEEDS_REVIEW because the required-Cl output formula and the altitude-to-density implementation are not explicitly specified, and the density data source is absent.

  • The lift-force formula L = ½ρV²ClS is standard and correct for steady aerodynamic lift when ρ is in kg/m³, V in m/s, S in m², and L is in newtons.
  • The claimed output 'required Cl for level flight given weight' has no formula in the spec. It should explicitly use Cl_required = W/(½ρV²S), where W is force in newtons.
  • The altitude-adjusted density calculation is underspecified: the spec references an ISA density table but provides neither the table, interpolation rule, altitude input definition, nor an alternative ISA formula.

Units and conventions

  • ρ is air density in kg/m³.
  • V must be in m/s before applying the formula; if entered in km/h, convert using V_m/s = V_km/h ÷ 3.6.
  • S is wing planform area in m².
  • Cl is dimensionless.
  • Lift force L and weight W are in newtons.
  • For level-flight Cl, required weight must be supplied as a force in newtons, not as mass in kilograms.

Inspectable vector

One of 4 source-bound review vectors:

{
  "inputs": {
    "Cl": 0.5,
    "S_m2": 16,
    "V_mps": 50,
    "rho_kg_m3": 1.225,
    "weight_N": 12000
  },
  "expected_outputs": {
    "lift_N": 12250,
    "required_Cl": 0.4897959184
  },
  "working": "Dynamic pressure q = ½ρV² = ½ × 1.225 × 50² = 0.6125 × 2500 = 1531.25 Pa. Lift L = q × Cl × S = 1531.25 × 0.5 × 16 = 1531.25 × 8 = 12250 N. Required Cl = W/(qS) = 12000/(1531.25 × 16) = 12000/24500 = 0.4897959184."
}

Failure boundary

BREAK_CLAIMED · SELF_FLAGGED

Required-Cl calculations divide by zero when V=0 or S=0 and must reject the input rather than emit a numeric result. The specification also provides no genuine formula branch, so signed negative velocity handling and the sign convention for lift and Cl remain ambiguous.

Other records

Sources and evidence

These pointers bind the page to evidence. They do not grant authority or collapse verification into deployment.

  • VERIFIED_LEDGER.json
  • evidence-tranche5/tranche5-results.json
  • BOUNDARY_HAZARD_CATALOG.json