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Help System Announcements PRINTER VERSION BACK NEXT ES Chapter 14, Problem X6 If the speed of...

Help System Announcements PRINTER VERSION BACK NEXT ES Chapter 14, Problem X6 If the speed of flow past the lower surface of

Help System Announcements PRINTER VERSION BACK NEXT ES Chapter 14, Problem X6 If the speed of flow past the lower surface of an airplane wing is 130 m/s, what speed of flow over the upper surface will give a pressure difference of 928 Pa between upper and lower surfaces? Take the density of air to be 1.30 x 10 g/cm2. Assume the lower surface is at the higher pressure. Number Units the tolerance is +/-2% Click if you would like to Show Work for this question: Open Show Work LINK TO TEXT LINK TO SAMPLE PROBLEM VIDEO MINI-LECTURE XE X4 Question Attempts: 0 of 5 used SAVE FOR LATER SUBMIT ANSWER ady
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Answer #1

Solution given U = 13omis S = 1.3 x10 glem AP = 928 Pa PL-Po = op Applied formale, gh & 1 6 6² = Constant thon L sgh+PU, P+ P

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