Title: Investigation of a nearly isentropic mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.2
Abstract: Wind tunnel tests of mixed-compression axisymmetric inlet system to determine bleed mass flow ratio, pressure recovery and pressure distortion
Publication Year: 1968
Publication Date: 1968-05-01
Language: en
Type: article
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Cited By Count: 3
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