Consider a circular cylinder of infinite span in a hypersonic flow. Using newtonian theory, show that the

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Consider a circular cylinder of infinite span in a hypersonic flow. Using newtonian theory, show that the drag coefficient based on cross-sectional area perpendicular to the flow is $4 / 3$.

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Modern Compressible Flow With Historical

ISBN: 9781260570823

4th Edition

Authors: John Anderson

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Question Posted: Apr 17, 2024 09:00 AM

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Consider a circular cylinder of infinite span in a hypersonic flow. Using newtonian theory, show that the

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Modern Compressible Flow With Historical

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