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

Edward C. B. DanforthJ. Ford Johnston

出版	National Advisory Committee for Aeronautics, 1949
URL	http://books.google.com.hk/books?id=nTsKywAACAAJ&hl=&source=gbs_api

註釋

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.