Step 1: General solution structure for harmonic forcing.
For a linear SDOF under \(m\ddot x + c\dot x + kx = F_0\sin\omega t\), the solution is
\[
x(t) = x_{\text{tr}}(t) + x_{\text{ss}}(t),
\]
where \(x_{\text{tr}}(t)\) is the homogeneous or free–vibration transient and \(x_{\text{ss}}(t)\) is the particular steady–state sinusoid at the forcing frequency.
\(\Rightarrow\) (A) is true.
Step 2: Behavior of the transient with damping.
If \(c>0\) (under/critical/over–damped), \(x_{\text{tr}}(t)\) carries an exponential factor \(e^{-\zeta\omega_n t}\) (or an overdamped sum of decaying exponentials), so it decays to zero as \(t\to\infty\).
\(\Rightarrow\) (B) is true. (Note: for \(c=0\) it would not decay, but that case is not listed.)
Step 3: Dependence of steady state on initial conditions.
\(x_{\text{ss}}(t)\) is determined solely by \(F_0,\omega,m,c,k\) through the FRF (magnitude \(X(\omega)\), phase \(\phi\)); it does not depend on initial displacement/velocity. Initial conditions only set the transient \(x_{\text{tr}}(t)\).
\(\Rightarrow\) (C) is false.
Step 4: Parameters controlling decay rate.
The decay envelope is \(e^{-\zeta\omega_n t}\) with \(\omega_n=\sqrt{k/m}\) and \(\zeta=\dfrac{c}{2m\omega_n}=\dfrac{c}{2\sqrt{km}}\). Thus the decay rate depends on \(m,k,c\).
\(\Rightarrow\) (D) is true.
Final Answer:
\[
\boxed{(A),\ (B),\ (D)}
\]
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).
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 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).