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        <datestamp>2026-10-02T18:45:45Z</datestamp>
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          <dc:title>ICAO Standard Atmosphere &amp; Density Altitude Computational Benchmark Matrix (6,885 Atmospheric Calculation Vectors)</dc:title>
          <dc:creator>Miad Saadidi (24671005)</dc:creator>
          <dc:subject>Aerospace engineering not elsewhere classified</dc:subject>
          <dc:subject>Atmospheric sciences not elsewhere classified</dc:subject>
          <dc:subject>icao 2017 ).</dc:subject>
          <dc:subject>atmospheric 3</dc:subject>
          <dc:description>&lt;p dir="ltr"&gt;### Summary&lt;/p&gt;&lt;p dir="ltr"&gt;This open dataset provides a high-resolution computational benchmark of 6,885 discrete thermodynamic atmospheric calculation vectors spanning geopotential altitudes from −1,000 ft to +20,000 ft MSL and ambient temperatures from −30°C to +50°C.&lt;/p&gt;&lt;p&gt;&lt;br&gt;&lt;/p&gt;&lt;p dir="ltr"&gt;Governed by ICAO Doc 7488/3 (*Manual of the ICAO Standard Atmosphere*) and the U.S. Standard Atmosphere (1976), this dataset evaluates non-linear atmospheric density ratio (σ) degradation and quantifies the divergence error of classical flight-training linear heuristics (such as the 120 ft/°C rule) against closed-form thermodynamic models.&lt;/p&gt;&lt;p&gt;&lt;br&gt;&lt;/p&gt;&lt;p dir="ltr"&gt;### Dataset Variables (11 Columns)&lt;/p&gt;&lt;p dir="ltr"&gt;1. `Elevation_ft`: Geopotential pressure altitude (−1,000 ft to +20,000 ft).&lt;/p&gt;&lt;p dir="ltr"&gt;2. `Temperature_C`: Ambient static air temperature (−30°C to +50°C).&lt;/p&gt;&lt;p dir="ltr"&gt;3. `ISA_Temperature_C`: Standard atmosphere temperature at elevation.&lt;/p&gt;&lt;p dir="ltr"&gt;4. `ISA_Deviation_C`: Temperature delta from standard atmosphere.&lt;/p&gt;&lt;p dir="ltr"&gt;5. `Pressure_Pa`: Static barometric air pressure in Pascals.&lt;/p&gt;&lt;p dir="ltr"&gt;6. `Density_kg_m3`: Air mass density in kilograms per cubic meter.&lt;/p&gt;&lt;p dir="ltr"&gt;7. `Density_Ratio_sigma`: Non-dimensional air density ratio (ρ / ρ₀).&lt;/p&gt;&lt;p dir="ltr"&gt;8. `Exact_Density_Altitude_ft`: Closed-form thermodynamic density altitude.&lt;/p&gt;&lt;p dir="ltr"&gt;9. `Heuristic_Density_Altitude_ft`: Linear 120-ft cockpit approximation.&lt;/p&gt;&lt;p dir="ltr"&gt;10. `DA_Error_ft`: Heuristic divergence error vector in feet.&lt;/p&gt;&lt;p dir="ltr"&gt;11. `TAS_Multiplier`: True airspeed correction multiplier (1 / √σ).&lt;/p&gt;&lt;p&gt;&lt;br&gt;&lt;/p&gt;&lt;p dir="ltr"&gt;### Interactive Tools &amp; Methodology&lt;/p&gt;&lt;p dir="ltr"&gt;- Interactive Web Version: https://aeroway.org/datasets/icao-standard-atmosphere-density-altitude-benchmark/&lt;/p&gt;&lt;p dir="ltr"&gt;- Student Laboratory (LAB-2026-01): https://aeroway.org/labs/density-altitude-and-performance/&lt;/p&gt;&lt;p dir="ltr"&gt;- Deterministic Calculator: https://aeroway.org/calculators/density-altitude-calculator/&lt;/p&gt;</dc:description>
          <dc:date>2026-10-02T18:45:45Z</dc:date>
          <dc:type>Dataset</dc:type>
          <dc:type>Dataset</dc:type>
          <dc:identifier>10.6084/m9.figshare.34059369.v1</dc:identifier>
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          <dc:rights>CC BY 4.0</dc:rights>
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