Error in Airspeed Measurement Due to Static-pressure Field Ahead of Sharp-nose Bodies of Revolution at Transonic Speeds

Error in Airspeed Measurement Due to Static-pressure Field Ahead of Sharp-nose Bodies of Revolution at Transonic Speeds

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As part of a study of means of airspeed measurement at transonic speed, studies have been made at Mach numbers up to 1.1 by the NACA wing-flow method of the static-pressure (or position) error ahead of two sharp-nose bodies of revolution at zero angle of attack.As part of a study of means of airspeed measurement at transonic speed, studies have been made at Mach numbers up to 1.1 by the NACA wing-flow method of the static-pressure (or position) error ahead of two sharp-nose bodies of revolution at ...


Title:Error in Airspeed Measurement Due to Static-pressure Field Ahead of Sharp-nose Bodies of Revolution at Transonic Speeds
Author: Edward C. B. Danforth, J. Ford Johnston, United States. National Advisory Committee for Aeronautics
Publisher: - 1949
ISBN-13:

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