The temperature and pressure at the stagnation point of a high-speed missile are 934R and 7.8atm, respectively.

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The temperature and pressure at the stagnation point of a high-speed missile are 934°R and 7.8atm, respectively. Calculate the density at this point.

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Dec 09, 2010 03:24 AM

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The temperature and pressure at the stagnation point of a high-speed missile are 934R and 7.8atm, respectively.

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Fundamentals of Aerodynamics

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