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Part A A jet plane is flying at M = 2.4, in air having a temperature of 2°C and absolute pressure of 80 kPa. The leading edge of the wing has an angle of 8 = 16°. (Figure 1) Determine the velocity of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. μÅ V = Value Units Submit Request Answer Figure 1 of 1 Part B ? M = 2.4 Determine the pressure of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. p = о ΜΑ ? Units Value Submit Request Answer Part C Determine the temperature of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer using three significant figures. ΕΠΙ ΑΣΦ Η vec VAΣ wwwww ? T = Submit Request Answer Part D K What is the angle & of the leading edge that will cause the shock wave to separate from the front of the wing? Express your answer using three significant figures. б= ΜΕ ΑΣΦ vec Submit Request Answer ?

Part A A jet plane is flying at M = 2.4, in air having a temperature of 2°C and absolute pressure of 80 kPa. The leading edge of the wing has an angle of 8 = 16°. (Figure 1) Determine the velocity of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. μÅ V = Value Units Submit Request Answer Figure 1 of 1 Part B ? M = 2.4 Determine the pressure of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. p = о ΜΑ ? Units Value Submit Request Answer Part C Determine the temperature of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer using three significant figures. ΕΠΙ ΑΣΦ Η vec VAΣ wwwww ? T = Submit Request Answer Part D K What is the angle & of the leading edge that will cause the shock wave to separate from the front of the wing? Express your answer using three significant figures. б= ΜΕ ΑΣΦ vec Submit Request Answer ?

Elements Of Electromagnetics
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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A jet plane is flying at M = 2.4, in air having a temperature of 2∘C and absolute pressure of 80 kPa. The leading edge of the wing has an angle of δ = 16∘. (Figure 1)
A. Determine the velocity of the air just in front or to the right of the oblique shock that forms on the wing.
B. Determine the pressure of the air just in front or to the right of the oblique shock that forms on the wing.
C. Determine the temperature of the air just in front or to the right of the oblique shock that forms on the wing.
D. What is the angle δδ of the leading edge that will cause the shock wave to separate from the front of the wing?

Part A A jet plane is flying at M = 2.4, in air having a temperature of 2°C and absolute pressure of 80 kPa. The leading edge of the wing has an angle of 8 = 16°. (Figure 1) Determine the velocity of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. μÅ V = Value Units Submit Request Answer Figure 1 of 1 Part B ? M = 2.4 Determine the pressure of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. p = о ΜΑ ? Units Value Submit Request Answer
Transcribed Image Text:Part A A jet plane is flying at M = 2.4, in air having a temperature of 2°C and absolute pressure of 80 kPa. The leading edge of the wing has an angle of 8 = 16°. (Figure 1) Determine the velocity of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. μÅ V = Value Units Submit Request Answer Figure 1 of 1 Part B ? M = 2.4 Determine the pressure of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer to three significant figures and include the appropriate units. p = о ΜΑ ? Units Value Submit Request Answer
Part C Determine the temperature of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer using three significant figures. ΕΠΙ ΑΣΦ Η vec VAΣ wwwww ? T = Submit Request Answer Part D K What is the angle & of the leading edge that will cause the shock wave to separate from the front of the wing? Express your answer using three significant figures. б= ΜΕ ΑΣΦ vec Submit Request Answer ?
Transcribed Image Text:Part C Determine the temperature of the air just in front or to the right of the oblique shock that forms on the wing. Express your answer using three significant figures. ΕΠΙ ΑΣΦ Η vec VAΣ wwwww ? T = Submit Request Answer Part D K What is the angle & of the leading edge that will cause the shock wave to separate from the front of the wing? Express your answer using three significant figures. б= ΜΕ ΑΣΦ vec Submit Request Answer ?
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