Consider an infinitely thin flat plate with a 5 m chord at an angle of attack of 5° in a supersonic flow. The pressure and shear stress distributions on the upper and lower surfaces are given by pu= 3 x 105 cos(TT x) + 4.9 x 105, pj= 6 x 105 cos(TT X) + 1.15 x 10°, Tu= 301x 0.4, and T/= 699x-0.4, respectively, where x is the distance from the leading edge in meters and p and 7 are in Newtons per square meter. Calculate the normal and axial forces, the lift and drag, moment about the leading edge, and moment about the one- quarter chord, all per unit span. Also, calculate the location of the center of pressure. (Round axial force to the nearest whole number and other answers to two decimal places.) Note: Do not use small-angle approximation. x 106 N/m. N/m. The normal force is The axial force is 106 105 N/m. The lift is N/m. The drag is

Consider an infinitely thin flat plate with a 5 m chord at an angle of attack of 5° in a supersonic flow. The pressure and shear stress distributions on the upper and lower surfaces are given by pu= 3 x 105 cos(TT x) + 4.9 x 105, pj= 6 x 105 cos(TT X) + 1.15 x 10°, Tu= 301x 0.4, and T/= 699x-0.4, respectively, where x is the distance from the leading edge in meters and p and 7 are in Newtons per square meter. Calculate the normal and axial forces, the lift and drag, moment about the leading edge, and moment about the one- quarter chord, all per unit span. Also, calculate the location of the center of pressure. (Round axial force to the nearest whole number and other answers to two decimal places.) Note: Do not use small-angle approximation. x 106 N/m. N/m. The normal force is The axial force is 106 105 N/m. The lift is N/m. The drag is

Principles of Geotechnical Engineering (MindTap Course List)

9th Edition

ISBN:9781305970939

Author:Braja M. Das, Khaled Sobhan

Publisher:Braja M. Das, Khaled Sobhan

Chapter10: Stresses In A Soil Mass

Section: Chapter Questions

Problem 10.12P: Refer to Figure 10.43. A strip load of q = 1450 lb/ft2 is applied over a width with B = 48 ft....

See similar textbooks

Similar questions

Refer to Figure P6.4. A strip load of q = 900 lb/ft2 is applied over a width B = 36 ft. Determine the increase in vertical stress at point A located z = 15 ft below the surface. Given: x = 27 ft.
A moment is exerted on the profile given in the figure to make an angle B with the vertical. Calculate the stress at point B. Given a = 90 mm, b = 60 mm, c = 110 mm, d = 130 mm, Beta = 80 degrees, M = 13 kNm,
I want Normal stress developed in segment AB. A homogeneous bar with a cross-sectional area of 400 mm2 is attached to fixed supports as shown inthe figure. It is subjected to lateral forces P1 = 20 kN and P2 = 50 kN. Determine the normal stressdeveloped in segments AB and BC. Answer: σAB = 80.55 MPa
H1. A rectangular beam of 100mm wide and 150mm deep is subjected to Shear force of 30KN, Determine ratio of Maximum shear stress to Average shear stress. Derive the equation which is used to find out the shear stress.
Refer to Figure P6.3. Determine the vertical stress increase Δσ at point A with the values q1 = 90 kN/m, q2 = 325 kN/m, x1 = 4 m, x2 = 2.5 m, and z = 3 m.
A newtonian fluid flows down an infinitely long cyalindrical tube (as shown in the figure below). There is NO applied pressure gradient, and fluid flows down the pipe due to gravity alone.i) Derive the velocity profile (?(?) =?). ii)Find???? ,???iii) Draw the velocity and shear stress profiles, showing the points where ? or ? is equal to zero or at their maximum value.
Determine the average axial tensile stress in the bar of the figure below if P=225 kN and the cross sectional area of the bar is 2500 square mm
Q#5: From the Tri –axial test, determine the effective normal stress on the plane of Maximum shear stress. Explain why the shear failure occurred along the plane with angle 54.73 and not along the plane of maximum shear stress. Take σ’1 = 552, σ’3 = 276, ø’ = 19.45? Find σ’ = ? τf = ? τ: ?
A hollow cylindrical steel shaft is 1.5 m long and has inner and outer diameters equal to 40 mm and 60 mm. (a) What is the largest torque which may be applied to the shaft if the shearing stress is not to exceed 120 MPa? (b) What is the corresponding minimum value of the shearing stress in the shaft?
Referring to Figure Q2 (a), the vertical stress increase at point A is 25 kN/m2due to application of line loads q1 and q2. Determine the magnitude of q2.
Q#5: From the Tri –axial test, determine the effective normal stress on the plane of Maximum shear stress. Explain why the shear failure occurred along the plane with angle 54.73 and not along the plane of maximum shear stress. Take σ’1 = 552, σ’3 = 276, ø’ = 19.45?
Find the expressions to calculate the maximum normal and shear stresses for a circular profile: d (diameter)= 0.30 m