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The temperature and pressure at the stagnation point of a high speed missile are 934 R and 7.8 atm. Find the answers.
The temperature and pressure at the stagnation point of a high speed missile are \({934^ \circ }\) R and 7.8 atm, …
Worldtech Asked on 26th December 2018 in Aeronautics.
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- 1 answers
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