Experimental Investigation Of A Large Scale Two Dimensional Mixed Compression Inlet System
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Experimental Investigation of a Large-scale, Two-dimensional, Mixed-compression Inlet System
A large scale, variable-geometry inlet system with a design Mach number of 3.0 was tested at Mach numbers from 0.6 to 1.28. Variable features for off-design operation are an adjustable-height ramp system and a translating cowl.