The Base Pressure Behind a Blunt Trailing Edge for Supersonic Two-Dimensional Flow. Approaching Streams Having the Same Stagnation Temperature but Dissimilar Mach Numbers and Stagnation Pressures
Tripp, Wilson
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https://hdl.handle.net/2142/57796
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The Base Pressure Behind a Blunt Trailing Edge for Supersonic Two-Dimensional Flow. Approaching Streams Having the Same Stagnation Temperature but Dissimilar Mach Numbers and Stagnation Pressures
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