m 13.111 vs at 700 m/s through a long duct in a wind tunnel, where the rature is 15° C and the absolute pressure is 65 kPa. The leading of a wing in the tunnel is represented by the 8° wedge. The angle of is set at a = 1.5°. (Figure 1) 700 m/s jα 1 of 1 Part A Determine the pressure created on its top surface. Express your answer to three significant figures a P= Value Submit μà Templates Provide Feedback Request Answer Units ?

Structural Analysis
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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Problem 13.111
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 65 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
700 m/s
4°
ja
4°
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
μA
Templates
Provide Feedback
Request Answer
Units
?
Transcribed Image Text:Problem 13.111 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 65 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 700 m/s 4° ja 4° 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 μA Templates Provide Feedback Request Answer Units ?
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