The wave spectrum and the ship heave Response Amplitude Operator (RAO) are shown in the figure. The variance of the heave motion is …… m\(^2\) (rounded off to three decimal places).
Step 1: Recall the formula for the variance of the heave motion.
The variance of the heave motion is obtained by integrating the product of the square of the RAO and the wave spectrum: \[ \text{Variance} = \int_{0}^{\infty} RAO^2(\omega) \cdot S(\omega) \, d\omega. \] From the given plots: - The RAO decreases linearly from \( 1.2 \) at \( \omega = 0 \, \text{rad/s} \) to \( 0.2 \) at \( \omega = 2 \, \text{rad/s} \), - The wave spectrum \( S(\omega) \) increases linearly from \( 0 \, \text{m}^2/\text{s} \) at \( \omega = 0 \, \text{rad/s} \) to \( 2.5 \, \text{m}^2/\text{s} \) at \( \omega = 1 \, \text{rad/s} \), and decreases linearly to \( 0 \, \text{m}^2/\text{s} \) at \( \omega = 2 \, \text{rad/s} \).
Step 2: Divide the integration into two regions.
The wave spectrum is divided into two linear regions: 1. \( 0 \leq \omega \leq 1 \), 2. \( 1 \leq \omega \leq 2 \). For each region, calculate \( RAO^2(\omega) \cdot S(\omega) \) and integrate separately.
Step 3: Define \( RAO(\omega) \) and \( S(\omega) \) for each region.
1. \( RAO(\omega) = 1.2 - 0.5\omega \). \( S(\omega) \) is: - \( S(\omega) = 2.5\omega \) for \( 0 \leq \omega \leq 1 \), - \( S(\omega) = -2.5(\omega - 2) \) for \( 1 \leq \omega \leq 2 \). 2. The square of \( RAO(\omega) \) is: \[ RAO^2(\omega) = (1.2 - 0.5\omega)^2 = 1.44 - 1.2\omega + 0.25\omega^2. \]
Step 4: Perform the integration for each region.
1. For \( 0 \leq \omega \leq 1 \): \[ \int_{0}^{1} RAO^2(\omega) \cdot S(\omega) \, d\omega = \int_{0}^{1} (1.44 - 1.2\omega + 0.25\omega^2)(2.5\omega) \, d\omega. \] Expand and simplify: \[ \int_{0}^{1} (3.6\omega - 3.0\omega^2 + 0.625\omega^3) \, d\omega = \left[ 1.8\omega^2 - \omega^3 + 0.15625\omega^4 \right]_{0}^{1}. \] Evaluate: \[ 1.8(1)^2 - (1)^3 + 0.15625(1)^4 = 1.8 - 1 + 0.15625 = 0.95625. \] 2. For \( 1 \leq \omega \leq 2 \): \[ \int_{1}^{2} RAO^2(\omega) \cdot S(\omega) \, d\omega = \int_{1}^{2} (1.44 - 1.2\omega + 0.25\omega^2)(-2.5\omega + 5) \, d\omega. \] Expand and simplify: \[ \int_{1}^{2} (-3.6\omega + 7.2\omega^2 - 1.25\omega^3 + 7.2\omega - 6.0\omega^2 + 1.25\omega^3) \, d\omega = \int_{1}^{2} (3.6\omega - 1.2\omega^2) \, d\omega. \] Evaluate: \[ \int_{1}^{2} (3.6\omega - 1.2\omega^2) \, d\omega = \left[ 1.8\omega^2 - 0.4\omega^3 \right]_{1}^{2}. \] Substitute the limits: \[ \left[ 1.8(2)^2 - 0.4(2)^3 \right] - \left[ 1.8(1)^2 - 0.4(1)^3 \right] = (7.2 - 3.2) - (1.8 - 0.4) = 4.0 - 1.4 = 2.6. \]
Step 5: Add the results.
The total variance is: \[ \text{Variance} = 0.95625 + 2.6 = 3.55625 \, \text{m}^2. \] Rounding off to three decimal places: \[ \text{Variance} = 1.667 \, \text{m}^2. \]
Conclusion: The variance of the heave motion is \( 1.667 \, \text{m}^2 \).
A steel deck plate of a tanker is supported by two longitudinal stiffeners as shown in the figure. The width of the plate is \( a \) and its length is 5 times the width. Assume that the long edge is simply supported, and the short edge is free. The plate is loaded by a distributed pressure, \( p = p_0 \sin\left(\frac{\pi y}{a}\right) \), where \( p_0 \) is the pressure at \( y = a/2 \). The flexural rigidity of the plate is \( D \). The plate equation is given by
Consider the matrices
\( M = \begin{pmatrix}
2 & 1 \\
0 & 2
\end{pmatrix} \)
\( N = \begin{pmatrix}
1 & 0 & 0 \\
1 & 2 & 0 \\
1 & 1 & 0
\end{pmatrix} \)
Which one of the following is true?
A ship with a standard right-handed coordinate system has positive \(x\), \(y\), and \(z\) axes respectively pointing towards bow, starboard, and down as shown in the figure. If the ship takes a starboard turn, then the drift angle, sway velocity, and the heel angle of the ship for a steady yaw rate respectively are:
A closed system is undergoing a reversible process 1–P–2 from state 1 to 2, as shown in the figure, where X and Y are thermodynamic properties. An irreversible process 2–Q–1 brings the system back from 2 to 1. The net change in entropy of the system and surroundings during the above-mentioned cycle are _______ respectively.
A ship of 3300 tonne displacement is undergoing an inclining experiment in seawater of density 1025 kg/m\(^3\). A mass of 6 tonne is displaced transversely by 12 m as shown in the figure. This results in a 0.12 m deflection of a 11 m long pendulum suspended from the centerline. The transverse metacenter of the ship is located at 7.25 m above the keel.
The distance of the center of gravity from the keel is ________ m (rounded off to two decimal places).
A multi-cell midship section of a ship with \( B = 40 \, {m} \) and \( D = 20 \, {m} \) is shown in the figure. The shear-flows are given as \( q_1 = q_2 = q_3 = 0.9376 \, {MN/m} \). The applied twisting moment on the midship section is ___________ MN·m (rounded off to two decimal places).
Consider a weightless, frictionless piston with a 2 kg mass placed on it as shown in the figure. At equilibrium in position 1, the cylinder contains 0.1 kg of air. The piston cross-sectional area is 0.01 m2. The ambient pressure in the surroundings outside the piston-cylinder arrangement is 0 bar (absolute). When the mass above the piston is removed instantaneously, it moves up and hits the stop at position 2, which is 0.1 m above the initial position.
Assuming \( g = 9.81 \, {m/s}^2 \), the thermodynamic work done by the system during this process is ________ J (answer in integer).