Hello, Please listen to me carefully. I need "What is the temperature of the Sun (google for the answer)? What is there-entry temperature of the Space Shuttle (google for the answer)? Whydon’t you burn up at the reentry temperature that you’ve calculated for thisMach 20 flow? The answer to this question will lead you to recognize thatFigure 4.6 is wrong and that the body should actually re-enter the Earth’satmosphere in the opposite direction. (ie.. blunt/flat surface first.)" to be answered based on the main question******Dont solve for the main question as I dont want it. ****** A body is reentering the earth's atmosphere at a Mach number of 20. In front of the bodyis a shockwave, as shown in Figure P4.6. Opposite the nose of the body, the shock can beseen 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 (neglectdissociation) with constant y = 1.4. The ambient pressure and temperature are 1.0 kPaand 220 K, respectively.Figure P4.6 What is the temperature of the Sun (google for the answer)? What is there-entry temperature of the Space Shuttle (google for the answer)? Whydon’t you burn up at the reentry temperature that you've calculated for thisMach 20 flow? The answer to this question will lead you to recognize thatFigure 4.6 is wrong and that the body should actually re-enter the Earth'satmosphere in the opposite direction. (ie.. blunt/flat surface first.)

given data,M1=20r=1.4P1=1kPaT1=220kM22=M12+2r-12rr-1 M12-1M22=2o2+21.4-12×1.41.4-1202-1

Answered: A body is reentering the earth's…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Hello,

Please listen to me carefully. I need "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.)" to be answered based on the main question

******Dont solve for the main question as I dont want it. ******

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.)

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