The report is useful in designing aircraft structures and in estimating aircraft performance. It provides data for use in aircraft strength and performance calculations for altitudes up to 32,000 meters (105,000 feet) and Mach numbers up to 3.0
True Airspeed in the International Standard Atmosphere and Equivalent Airspeed Corresponding to Mach Number and Pressure Altitude
1978
9 pages
Report
Keine Angabe
Englisch
Simplified chart for determining Mach Number and true airspeed from airspeed-indicator readings
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