For a three-bar truss loaded as shown in the figure, the magnitude of the force in the horizontal member AB is __________ N (answer in integer).
We are asked to determine the force in the horizontal member \( AB \) of the truss, which can be done using the method of joints or the method of sections. Since the truss is symmetrical, we can simplify the analysis by using equilibrium equations.
Step 1: Identify the forces and equilibrium.
Let \( F_{AB} \) be the force in the horizontal member \( AB \). The truss is loaded with a 50 N force applied vertically at joint \( C \). Since the truss is symmetrical, the forces in members \( AC \) and \( BC \) will be equal. At joint \( C \), we can set up the equilibrium equations for both the horizontal and vertical directions. The vertical force at joint \( C \) is balanced by the force components of members \( AC \) and \( BC \). The horizontal force at joint \( C \) is balanced by the force in the horizontal member \( AB \).
Step 2: Use equilibrium equations.
For vertical equilibrium at joint \( C \): \[ 2 F_{AC} \sin 45^\circ = 50 \quad \Rightarrow \quad F_{AC} = \frac{50}{2 \sin 45^\circ} = \frac{50}{\sqrt{2}} \approx 35.36 \, {N} \] For horizontal equilibrium at joint \( C \): \[ F_{AB} = F_{AC} \cos 45^\circ = 35.36 \times \cos 45^\circ \approx 35.36 \times 0.707 \approx 25 \, {N} \] Thus, the magnitude of the force in the horizontal member \( AB \) is 25 N.
A prismatic vertical column of cross-section \( a \times 0.5a \) and length \( l \) is rigidly fixed at the bottom and free at the top. A compressive force \( P \) is applied along the centroidal axis at the top surface. The Young’s modulus of the material is 200 GPa and the uniaxial yield stress is 400 MPa. If the critical value of \( P \) for yielding and for buckling of the column are equal, the value of \( \frac{l}{a} \) is __________ (rounded off to one decimal place).
For a three-bar truss loaded as shown in the figure, the magnitude of the force in the horizontal member AB is ____________ N (answer in integer).

A prismatic vertical column of cross-section \( a \times 0.5a \) and length \( l \) is rigidly fixed at the bottom and free at the top. A compressive force \( P \) is applied along the centroidal axis at the top surface. The Young’s modulus of the material is 200 GPa and the uniaxial yield stress is 400 MPa. If the critical value of \( P \) for yielding and for buckling of the column are equal, the value of \( \frac{l}{a} \) is ____________ (rounded off to one decimal place).

For a three-bar truss loaded as shown in the figure, the magnitude of the force in the horizontal member AB is _________ N (answer in integer).

Two designs A and B, shown in the figure, are proposed for a thin-walled closed section that is expected to carry only torque. Both A and B have a semi-circular nose, and are made of the same material with a wall thickness of 1 mm. With strength as the only criterion for failure, the ratio of maximum torque that B can support to the maximum torque that A can support is _________ (rounded off to two decimal places).
A thin flat plate is subjected to the following stresses: \[ \sigma_{xx} = 160 \, {MPa}; \, \sigma_{yy} = 40 \, {MPa}; \, \tau_{xy} = 80 \, {MPa}. \] Factor of safety is defined as the ratio of the yield stress to the applied stress. The yield stress of the material under uniaxial tensile load is 250 MPa. The factor of safety for the plate assuming that material failure is governed by the von Mises criterion is _________ (rounded off to two decimal places).
A uniform rigid bar of mass 3 kg is hinged at point F, and supported by a spring of stiffness \( k = 100 \, {N/m} \), as shown in the figure. The natural frequency of free vibration of the system is ___________ rad/s (answer in integer).
A jet-powered airplane is steadily climbing at a rate of 10 m/s. The air density is 0.8 kg/m³, and the thrust force is aligned with the flight path. Using the information provided in the table below, the airplane’s thrust to weight ratio is ___________ (rounded off to one decimal place). 
F and G denote two points on a spacecraft’s orbit around a planet, as indicated in the figure. O is the center of the planet, P is the periapsis, and the angles are as indicated in the figure. If \( OF = 8000 \, {km} \), \( OG = 10000 \, {km} \), \( \theta_F = 0^\circ \), and \( \theta_G = 60^\circ \), the eccentricity of the spacecraft's orbit is __________ (rounded off to two decimal places).