PhysicsI need help solving question number 1 please Problem 1:As shown in Fig. 1(a), a flat-plate airfoil with a chord length c has an angle of attack, a..Surface pressures on the lower and upper surfaces are p1 and p2, respectively.Calculate the lift and drag of the flat-plate airfoil.Note: Decompose pressure vectors into the vertical and horizontal components thatcontribute to the lift and drag, respectively.Problem 2:As shown in Fig. 1(b), a two-segment airfoil with a chord length c has a slope angle a..Surface pressures on the two upper surfaces are p1 and p3, respectively. The pressure onthe lower surface is p2.Calculate the lift and drag of the flat-plate airfoil.Note: Decompose pressure vectors into the vertical and horizontal components thatcontribute to the lift and drag, respectively. The chord length c is a distance between theleading and trailing edges. You need to calculate the length of a segment.a(a)plp2p2apl(b)p3

In the given image in question, a flat-plate airfoil with a chord length c has an angle of attack..…

Problem 1: As shown in Fig. 1(a), a flat-plate airfoil with a chord length c has an angle of attack, a.. Surface pressures on the lower and upper surfaces are p1 and p2, respectively. Calculate the lift and drag of the flat-plate airfoil. Note: Decompose pressure vectors into the vertical and horizontal components that contribute to the lift and drag, respectively.

Problem 1: As shown in Fig. 1(a), a flat-plate airfoil with a chord length c has an angle of attack, a.. Surface pressures on the lower and upper surfaces are p1 and p2, respectively. Calculate the lift and drag of the flat-plate airfoil. Note: Decompose pressure vectors into the vertical and horizontal components that contribute to the lift and drag, respectively.

Physics for Scientists and Engineers: Foundations and Connections

1st Edition

ISBN:9781133939146

Author:Katz, Debora M.

Publisher:Katz, Debora M.

Chapter15: Fluids

Section: Chapter Questions

Problem 22PQ: A spherical submersible 2.00 m in radius, armed with multiple cameras, descends under water in a...

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Problem 1: As shown in Fig. 1(a), a flat-plate airfoil with a chord length c has an angle of attack, a.. Surface pressures on the lower and upper surfaces are p1 and p2, respectively. Calculate the lift and drag of the flat-plate airfoil. Note: Decompose pressure vectors into the vertical and horizontal components that contribute to the lift and drag, respectively. Problem 2: As shown in Fig. 1(b), a two-segment airfoil with a chord length c has a slope angle a.. Surface pressures on the two upper surfaces are p1 and p3, respectively. The pressure on the lower surface is p2. Calculate the lift and drag of the flat-plate airfoil. Note: Decompose pressure vectors into the vertical and horizontal components that contribute to the lift and drag, respectively. The chord length c is a distance between the leading and trailing edges. You need to calculate the length of a segment. a (a) pl p2 p2 a pl (b) p3
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