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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