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 95 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) Figure 1 of 1 > Part A Determine the pressure created on its top surface. Express your answer to three significant figures and include the appropriate units. μÅ P= Value Submit Request Answer Provide Feedback Units ? Next >
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 95 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) Figure 1 of 1 > Part A Determine the pressure created on its top surface. Express your answer to three significant figures and include the appropriate units. μÅ P= Value Submit Request Answer Provide Feedback Units ? Next >
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
Air flows at 700 m/sm/s through a long duct in a wind tunnel, where the temperature is 15∘C∘C and the absolute pressure is 95 kPakPa . 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.
Express your answer to three significant figures and include the appropriate units.

Transcribed Image Text: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 95 kPa. The leading edge of a wing in the tunnel is
represented by the 8º wedge. The angle of attack is set at
a = 1.5°. (Figure 1)
Figure
1 of 1
Part A
Determine the pressure created on its top surface.
Express your answer to three significant figures and include the
appropriate units.
p=
Value
Submit
HÁ
Provide Feedback
Request Answer
Units
?
Next >
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