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The Quarterly Journal of Mechanics and Applied Mathematics 1962 15(4):487-508; doi:10.1093/qjmam/15.4.487
© 1962 by Oxford University Press
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TRANSONIC FLOW IN TWO-DIMENSIONAL AND AXIALLY-SYMMETRIC NOZZLES

I. M. HALL

( Mechanics of Fluids Department, Manchester University )

By means of suitable expansions in inverse powers of R, the radius of curvature of the nozzle profile at the throat measured in throat half-heights, the velocity components in the throat region of a convergent-divergent nozzle can be calculated. The first three terms of the series solution have been obtained both for two-dimensional and for axially-symmetrie nozzles. The numerical accuracy of the solution is confirmed by comparison with the known exact solution along the branchline.


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