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A Shortened Method for the Calculation of Aerofoil Profile Drag*
Published online by Cambridge University Press: 28 July 2016
Summary
A rapid method is developed for estimating the profile drag of an aerofoil with a known transition point position. The results are in good agreement with previous calculations.
- Type
- Research Article
- Information
- Copyright
- Copyright © Royal Aeronautical Society 1952
Footnotes
An extract from College of Aeronautics Report No. 35.
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