- Nonlinear elastic \(\Rightarrow\) nonlinear curve but identical loading and unloading paths.
- Homogeneous \(\Rightarrow\) properties are independent of position.
- Isotropic \(\Rightarrow\) properties independent of direction, so infinite symmetry planes.
- Linear elastic \(\Rightarrow\) straight line stress-strain with no hysteresis.
The stress-strain graph for a nonlinear elastic material is as shown in the figure. 
The stress-strain graph for a linear elastic material is as shown in the figure. 
Step 1: Check option (A).
A nonlinear elastic material has a nonlinear stress-strain curve, but unloading follows the same path as loading (no hysteresis). The figure shown has different loading and unloading paths, which corresponds to inelastic or plastic behavior, not nonlinear elasticity.
\(\Rightarrow\) (A) is incorrect.
Step 2: Check option (B).
By definition, a homogeneous material has properties independent of position. Hence material constants are the same at all points in the body.
\(\Rightarrow\) (B) is correct.
Step 3: Check option (C).
An isotropic material has identical properties in all directions. This implies infinitely many planes of symmetry because the material response does not depend on orientation.
\(\Rightarrow\) (C) is correct.
Step 4: Check option (D).
A linear elastic material follows Hooke's law: stress is proportional to strain. This gives a straight-line stress-strain curve, and loading and unloading occur along the same line. The figure shown for (D) is correct.
\(\Rightarrow\) (D) is correct.
\[\boxed{\text{Correct options: (B), (C), (D)}}\]
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).
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 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).