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Static Thrust of an Annular Nozzle with a Concave Central Base (1960)

Mercer, Charles E. ; Corson, Blake W., Jr.

In: CASI

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Publication Date: 2019-08-17

Description: A static test of an annular nozzle with a concave central base, producing a jet in which tangents to the jet streamlines at the exit converged toward a region on the axis of symmetry downstream of the exit, has indicated good thrust performance. A value of nozzle-flow coefficient only slightly less than unity indicates the internal loss to be small. Pressures on the concave central base are relatively large and positive, and a predictable portion of the total thrust of the jet is exerted on the central base.

Keywords: Aircraft Propulsion and Power

Type: NASA-TN-D-418 , L-851

Format: application/pdf

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