Download Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system: Internal performance and drag at transonic conditions, free stream Mach equals 0.6 to 1.28 Hardcover
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Experimental investigation of a large-scale,
free stream Mach equals 0.6 to 1.28,
mixed-compression inlet system: Internal performance and drag at transonic conditions,
two-dimensional
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