NASA NTRS · 20030065295
Design Data for Graphical Construction of Two-Dimensional Sharp-Edge-Throat Supersonic Nozzles
Abstract
Design data are presented for the graphical construction of two-dimensional sharp-edge-throat supersonic nozzles of minimum length for test-section Mach numbers from 1.20 to 10.00. The method of characteristics used in the design is briefly reviewed.
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Shames, Harold, Seashore, Ferris L.. 1948-12-02. Design Data for Graphical Construction of Two-Dimensional Sharp-Edge-Throat Supersonic Nozzles. https://ntrs.nasa.gov/citations/20030065295
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