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Theses and Dissertations
Barrett, The Honors College Thesis/Creative Project Collection
Design and Analyze a Liquid-Liquid Swirl Coaxial Injector for a small-scale rocket engine using Computational Fluid Dynamics for minimum pressure drop and maximum spray angle.
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Design and Analyze a Liquid-Liquid Swirl Coaxial Injector for a small-scale rocket engine using Computational Fluid Dynamics for minimum pressure drop and maximum spray angle.
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abstract.pdf
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abstract.pdf
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abstract.pdf
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Dave_H_Spring_2019.pdf
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Dave_H_Spring_2019.pdf
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Dave_H_Spring_2019.pdf
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