An investigation was conducted in the static-test facility of the Langley 16-Foot Transonic Tunnel to determine the internal performance of a high-aspect-ratio nonaxisymmetric nozzle with five circular-to-rectangular transition ducts of varying design. Nozzle pressure ratio was varied from 1.5 to 5.3, and nozzle performance parameters were recorded.
Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
1986-03-01
Report
No indication
English
Computational Investigation of Circular-to-Rectangular Transition Ducts
Online Contents | 1994
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