A jet plane is flying in air that has a temperature of 2°C and absolute pressure of 85 kPa. The leading edge of the wing has the wedge shape shown. The plane has a speed of 800 m/s and the angle of attack is 2°. (Figure 1) Figure 13° 3° Ta = 2° < 1 of 1 ▾ Determine the pressure of the air at the lower surface B just in front or to the right of the oblique shock wave that forms at the leading edge. Express your answer to three significant figures and include the appropriate units. PB = Value Submit Part B. μÃ To= Submit Request Answer Determine the temperature of the air at the lower surface B just in front or to the right of the oblique shock wave that forms at the leading edge. Express your answer using three significant figures. 196,ΑΣΦ 4th Ivec Request Answer ⒸI ? < Return to Assignment Units Provide Feedback C IWC ? K

A jet plane is flying in air that has a temperature of 2°C and absolute pressure of 85 kPa. The leading edge of the wing has the wedge shape shown. The plane has a speed of 800 m/s and the angle of attack is 2°. (Figure 1) Figure 13° 3° Ta = 2° < 1 of 1 ▾ Determine the pressure of the air at the lower surface B just in front or to the right of the oblique shock wave that forms at the leading edge. Express your answer to three significant figures and include the appropriate units. PB = Value Submit Part B. μÃ To= Submit Request Answer Determine the temperature of the air at the lower surface B just in front or to the right of the oblique shock wave that forms at the leading edge. Express your answer using three significant figures. 196,ΑΣΦ 4th Ivec Request Answer ⒸI ? < Return to Assignment Units Provide Feedback C IWC ? K

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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Question

A jet plane is flying in air that has a temperature of 2°C and absolute pressure of 85 kPa. The
leading edge of the wing has the wedge shape shown. The plane has a speed of 800 m/s and
the angle of attack is 2º. (Figure 1)
Figure
B
13°
3⁰
Ta = 2°
< 1 of 1
▼
Pall A
Determine the pressure of the air at the lower surface B just in front or to the right of the oblique shock wave that forms at the leading edge.
Express your answer to three significant figures and include the appropriate units.
PB =
Submit
Part B
TB =
μÅ
Submit
Value
Request Answer
Determine the temperature of the air at the lower surface B just in front or to the right of the oblique shock wave that forms at the leading edge.
Express your answer using three significant figures.
VAE Ivec
Request Answer
→
< Return to Assignment
Units
n
?
Provide Feedback
BE
?
K

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