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Beckwith, Ivan E.
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1403844
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Beckwith, Ivan E.
Beckwith Ivan E.
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An accurate and rapid method for the design of supersonic nozzles
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Detailed description and results of a method for computing mean and fluctuating quantities in turbulent boundary layers
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The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section
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