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Note: this form uses JavaScript to compute properties related to the 1976 standard atmosphere up to 230,000 ft. The computations require Netscape 2.0 or later.
Adapted by Andrew McGrath from calculator by Ilam Kroo, Stanford University.

Select unit system: Metric Imperial

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Inputs

Altitude
Speed
Reference Length

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Results

Temperature
Density
Pressure
Speed of Sound
Viscosity
Mach Number
Dynamic Pressure
Critical Cp
Vacuum Cp
Reynolds Number
Laminar Cf
Turbulent Cf

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