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CALCULATIONS FOR THE DESIGN OF NOZZLES.
ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)
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Details are given of the numerical procedures required in the design of an axially-symmetric nozzle. A velocity distribution along the axis of symmetry is assumed to be given and from this, a characteristic network is used to determine the isentropic core boundary after which a boundary layer calculation gives the shape of the nozzle itself. Author
APPROVED FOR PUBLIC RELEASE