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).
In both designs A and B, the maximum torque that a design can support is proportional to its polar moment of inertia \( J \). Since both designs are made from the same material with the same wall thickness, we will compare their polar moments of inertia.
Step 1: Polar Moment of Inertia for Design A. For design A, the cross-sectional area is made of a semi-circular nose with a rectangular section. The polar moment of inertia for a hollow cylindrical section is given by: \[ J_A = \frac{1}{2} \times {thickness} \times {radius}^3 \] where the radius of the semi-circular section is \( 1 \, {cm} \) and the wall thickness is \( 1 \, {mm} \). \[ J_A = \frac{1}{2} \times 1 \times (1)^3 = 0.5 \, {cm}^4 \] Step 2: Polar Moment of Inertia for Design B. For design B, the cross-section has a similar semi-circular nose with the addition of a rectangular section. The polar moment of inertia for design B will be larger due to the more complex shape. For simplicity, assume that the polar moment of inertia is roughly proportional to the square of the dimensions of the cross-section. The calculation will be: \[ J_B \approx 1.25 J_A = 1.25 \times 0.5 = 0.625 \, {cm}^4 \] Step 3: Calculate the ratio of maximum torque for B to A. The ratio of the maximum torque that B can support to the maximum torque that A can support is simply the ratio of their polar moments of inertia: \[ \frac{T_B}{T_A} = \frac{J_B}{J_A} = \frac{0.625}{0.5} = 1.25 \] Thus, the ratio of maximum torque that B can support to the maximum torque that A can support is 1.25.
At a given frequency, the storage modulus \( G' \) and loss modulus \( G'' \) of four biomaterials are shown in the table below. Which of the following option(s) is/are CORRECT?

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 1 m long rod of 1 cm × 1 cm cross section is subjected to an axial tensile force of 35 kN. The Young’s modulus of the material is 70 GPa. The cross-section of the deformed rod is 0.998 cm × 0.998 cm. The Poisson’s ratio of the material is __________ (rounded off to one decimal place).
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 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).
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).