Wind Load on Flag Area Calculator

Restrictedquasisteadyrigid-equivalentdrag.5ρU²CdA,flagfluttergusts/pole/leverage omitted,no safe poleloadcertification. Actual independently applicable flag/cloth/manufacturer/jurisdiction/protocol/sourceedition,units/calibration and observations external;not legal/display precedence,authenticity,visibility or structural safety approval.

Description

Wind load links air density, speed, exposed area and drag coefficient.

Wind load links air density, speed, exposed area and drag coefficient.1

This calculation treats the flag as a steady equivalent surface, so flutter, gusts and pole leverage require separate analysis.

When to use Wind Load on Flag Area Calculator

Use this tool to apply the stated wind load on flag area calculator operation with an explicit input and unit basis.

How to use Wind Load on Flag Area Calculator and how it works

  1. Establish the measurement basis and units described above.
  2. Enter actualAirDensityKgPerM3, actualWindSpeedMps, actualProjectedFlagAreaM2, callerIndependentApplicableDragCoefficient and run the tool.
  3. Read result.value using the output meanings below.
  4. If input is rejected, correct the stated type, range, ordering or alignment issue and rerun; review successful results under the declared convention.
Input fieldMeaningValue typeRequirement
actualAirDensityKgPerM3Air density kg per m3, on the basis specified in the algorithm.numberrequired; finite; strictly positive; further conditions in the algorithm
actualWindSpeedMpsWind speed mps, on the basis specified in the algorithm.numberrequired; finite; nonnegative; further conditions in the algorithm
actualProjectedFlagAreaM2Projected flag area m2, on the basis specified in the algorithm.numberrequired; finite; nonnegative; further conditions in the algorithm
callerIndependentApplicableDragCoefficientDrag coefficient, on the basis specified in the algorithm.numberrequired; finite; nonnegative; further conditions in the algorithm

Require positive density and nonnegative speed, projected area and drag coefficient. Evaluate one-half density times speed squared times area times coefficient; coherent SI inputs produce newtons.

force = 0.5 × ρ × U² × A × Cd

Apply the declared units, ordering and branch conditions.

Output fieldMeaningValue type
resultObject containing the declared output fields.object
result.valueSteady equivalent drag force in newtons for coherent SI inputs.number
json
{
  "input": {
    "actualAirDensityKgPerM3": 1,
    "actualWindSpeedMps": 2,
    "actualProjectedFlagAreaM2": 1,
    "callerIndependentApplicableDragCoefficient": 1
  },
  "output": {
    "result": {
      "value": 2
    }
  }
}

Limitations and assumptions

The output applies the declared operation to the values you supply. Establish the measurement basis, units, coefficients and any caller-selected rules before interpreting it. The tool does not independently collect or verify observations or decide whether a model or reference applies. The simplified geometry or force calculation does not establish structural capacity, flotation stability or safe travel conditions.

Supply explicit required fields with the documented types and dense aligned arrays. Unknown fields, wrong types and nonfinite numbers are rejected. Branch-specific constraints are explained above. A successful false boolean, negative signed difference, empty slice or unresolved tie is distinct from an input error. Very large inputs or outputs may be rejected by shared resource limits.

Alternative or Complementary methods

For a related operation, use Recommended Flagpole Height by Flag Size Lookup. A flag size and pole height must be considered with the pole system, wind exposure and manufacturer guidance.

For a related operation, use Flag Size by Pole Height Recommendation Lookup. Selecting a flag size for a pole requires the actual pole system, material and wind exposure.

References

  1. Wind Load on Flag Area Calculator — tool.io

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