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The Pressure Rise with Subsonic Mach Number on Fuselages and Nacelles
Published online by Cambridge University Press: 28 July 2016
Extract
In treating the compressible subsonic flow by the Prandtl-Glauert method as extended by Göthert, the velocity increment v in the direction of the main stream is found to be 1/β2 times the corresponding velocity increment va on the analogous body in incompressible flow; the analogous body being obtained by reducing the lateral dimensions of the real body in the ratio β:1.
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- Copyright © Royal Aeronautical Society 1954