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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. Danforth
J. 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.