Converts airspeed values between calibrated airspeed (CAS), true airspeed (TAS), and Mach number using the ICAO Standard Atmosphere model, with corrections for non-standard temperature. Includes corrections for supersonic flow.
Features:
- Numerical or graphical conversion
- Pressure altitude ranges from sea level to 100,000 feet
- Handles up to Mach 5 in calculations
- Choose feet or meters for altitude input, and Celsius or Fahrenheit for temperature input
- Set the output precision of the displayed data
- Brief description of operation and usage of the app
NOT FOR FLIGHT CRITICAL OPERATIONS