Part A Air flows at 700 m/s through a long duct in a wind tunnel, where the temperature is 15° C and the absolute pressure is 70 kPa. The leading edge of a wing in the tunnel is represented by the 8° wedge. The angle of attack is set at a 1.5°. (Figure 1) = Determine the pressure created on its top surface. Express your answer to three significant figures and include the appropriate units. Figure 4° 700 m/s 4° ☐ ° Α p = Value 1 of 1 Submit Request Answer Provide Feedback Units ?
Part A Air flows at 700 m/s through a long duct in a wind tunnel, where the temperature is 15° C and the absolute pressure is 70 kPa. The leading edge of a wing in the tunnel is represented by the 8° wedge. The angle of attack is set at a 1.5°. (Figure 1) = Determine the pressure created on its top surface. Express your answer to three significant figures and include the appropriate units. Figure 4° 700 m/s 4° ☐ ° Α p = Value 1 of 1 Submit Request Answer Provide Feedback Units ?
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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Air flows at 700 m/s through a long duct in a wind tunnel, where the temperature is 15∘C and the absolute pressure is 70 kPa . The leading edge of a wing in the tunnel is represented by the 8∘ wedge. The angle of attack is set at α = 1.5∘. (Figure 1)
Determine the pressure created on its top surface.

Transcribed Image Text:Part A
Air flows at 700 m/s through a long duct in a wind tunnel,
where the temperature is 15° C and the absolute pressure is
70 kPa. The leading edge of a wing in the tunnel is
represented by the 8° wedge. The angle of attack is set at
a 1.5°. (Figure 1)
=
Determine the pressure created on its top surface.
Express your answer to three significant figures and include the appropriate units.
Figure
4°
700 m/s
4°
☐
°
Α
p =
Value
1 of 1
Submit
Request Answer
Provide Feedback
Units
?
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