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


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    Title :

    True Airspeed in the International Standard Atmosphere and Equivalent Airspeed Corresponding to Mach Number and Pressure Altitude


    Publication date :

    1978


    Size :

    9 pages



    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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