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The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59119

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The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.592345233

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LD5655.V855_1962.A549.pdf60

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