Title: Investigation of a variable Mach number supersonic tunnel with nonintersecting characteristics
Abstract: Report presenting a method for the design of supersonic-wind-tunnel nozzles that produce uniform flow over a continuously variable Mach number range without the use of flexible walls. Experimental results from a preliminary investigation of the tunnel are included, including calibration survey of flow, Mach number distributions, and pressure gradients are provided.
Publication Year: 1948
Publication Date: 1948-11-15
Language: en
Type: article
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Cited By Count: 3
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