stagnati ure tempe re to which the nose is subjected. Assume that the air behaves as a perfect gas (neglect ssociation) with constant y = 1.4. The ambient pressure and temperature are 1.0 kPa ad 220 K, respectively. Figure P4.6

Elements Of Electromagnetics
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Please only answer STEP 2 question. THIS IS MY 3RD TIME POSTING THE SAME QUESTION AND NOT GETTING THE ANSWER I NEED. DONT SOLVE FOR THE MAIN QUESTION, I NEED THE ANSWER TO THE SECOND PART OF THE QUESTION ONLY.

A body is reentering the earth's atmosphere at a Mach number of 20. In front of the body
is a shockwave, as shown in Figure P4.6. Opposite the nose of the body, the shock can be
seen to be normal to the flow direction. Determine the stagnation pressure and tempera-
ture to which the nose is subjected. Assume that the air behaves as a perfect gas (neglect
dissociation) with constant y = 1.4. The ambient pressure and temperature are 1.0 kPa
and 220 K, respectively.
Figure P4.6
Transcribed Image Text:A body is reentering the earth's atmosphere at a Mach number of 20. In front of the body is a shockwave, as shown in Figure P4.6. Opposite the nose of the body, the shock can be seen to be normal to the flow direction. Determine the stagnation pressure and tempera- ture to which the nose is subjected. Assume that the air behaves as a perfect gas (neglect dissociation) with constant y = 1.4. The ambient pressure and temperature are 1.0 kPa and 220 K, respectively. Figure P4.6
What is the temperature of the Sun (google for the answer)? What is the
re-entry temperature of the Space Shuttle (google for the answer)? Why
don’t you burn up at the reentry temperature that you've calculated for this
Mach 20 flow? The answer to this question will lead you to recognize that
Figure 4.6 is wrong and that the body should actually re-enter the Earth's
atmosphere in the opposite direction. (ie.. blunt/flat surface first.)
Transcribed Image Text:What is the temperature of the Sun (google for the answer)? What is the re-entry temperature of the Space Shuttle (google for the answer)? Why don’t you burn up at the reentry temperature that you've calculated for this Mach 20 flow? The answer to this question will lead you to recognize that Figure 4.6 is wrong and that the body should actually re-enter the Earth's atmosphere in the opposite direction. (ie.. blunt/flat surface first.)
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