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Transonic Similarity Correlation of the Terminal Shock Jump on Aerofoils
Published online by Cambridge University Press: 04 July 2016
Extract
This note illustrates the correlation of the pressure distributions measured on three NACA 16-series aerofoils at subsonic and transonic speeds. The transonic similarity parameters proposed by Spreiter
are used for the subsonic, transonic and supersonic types of flow illustrated in Fig. 1.
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- Copyright © Royal Aeronautical Society 1964