Problem 13.111Air flows at 700 m/s through a long duct in a wind tunnel, where thetemperature is 15° C and the absolute pressure is 65 kPa. The leadingedge of a wing in the tunnel is represented by the 8° wedge. The angle ofattack is set at a = 1.5°. (Figure 1)Figure700 m/s4°ja4°1 of 1Part ADetermine the pressure created on its top surface.Express your answer to three significant figures and include the appropriate units.p= ValueSubmitμATemplatesProvide FeedbackRequest AnswerUnits?

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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 μÃ Templates Provide Feedback Request Answer Units ?

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 μÃ Templates Provide Feedback Request Answer Units ?

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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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
?

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