Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section

John C. Evvard, Stephen H. Maslen
naca-tn-2688
Apr 1952


A method is presented for obtaining three-dimensional unsymmetric supersonic nozzles and inlets from known axisymmetric flows. Streamlines bounding the desired exit shape are traced through the known basic flow solution to give the required unsymmetric wall contours. Several examples are given.

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