We are given:
- Initial volume \( V_1 = 0.01 \, {kg} \times 0.020602 \, {m}^3/{kg} = 0.00020602 \, {m}^3 \),
- Initial pressure \( p_1 = 1 \, {MPa} \),
- Final pressure \( p_2 = 0.35 \, {MPa} \),
- The displacement of the piston is 50 mm.
The relation between pressure and specific volume is given as: \[ p v^n = {constant} \] where \( n \) is the polytropic index.
Step 1: We first calculate the initial volume \( V_1 \) using the formula: \[ V_1 = m \times v_1 = 0.01 \, {kg} \times 0.020602 \, {m}^3/{kg} = 0.00020602 \, {m}^3 \] Step 2: The diameter of the piston is given as \( d = 250 \, {mm} = 0.25 \, {m} \). The cross-sectional area of the piston is: \[ A = \frac{\pi d^2}{4} = \frac{\pi (0.25)^2}{4} = 0.0491 \, {m}^2 \] The volume displaced by the piston is: \[ \Delta V = A \times \Delta h = 0.0491 \, {m}^2 \times 0.05 \, {m} = 0.002455 \, {m}^3 \] Step 3: The final volume \( V_2 \) is the sum of the initial volume and the volume displaced: \[ V_2 = V_1 + \Delta V = 0.00020602 + 0.002455 = 0.00266102 \, {m}^3 \] Step 4: The relation \( p v^n = {constant} \) implies: \[ p_1 V_1^n = p_2 V_2^n \] Substitute the known values: \[ 1000 \times (0.00020602)^n = 350 \times (0.00266102)^n \] \[ \frac{1000}{350} = \left( \frac{0.00266102}{0.00020602} \right)^n \] \[ 2.8571 = \left( 12.9 \right)^n \] Step 5: Now, solve for \( n \) by taking the logarithm of both sides: \[ \log(2.8571) = n \log(12.9) \] \[ n = \frac{\log(2.8571)}{\log(12.9)} = \frac{0.456} {1.110} = 1.30 \] Step 6: Therefore, the value of the exponent \( n \) is approximately 1.30, which is within the given range.
A stream of superheated steam (2 MPa, 300°C) mixes with another stream of superheated steam (2 MPa, 400°C) through a steady-state adiabatic process. The flow rates of the streams are 3 kg/min and 2 kg/min, respectively. This mixture then expands in an adiabatic nozzle to a saturated mixture with quality of 0.77 and 1 kPa. Neglect the velocity at the nozzle entrance and the change in potential energies. The velocity at the nozzle exit (in m/s) is ......... (rounded off to two decimal places).
Use the following data:
At 2 MPa, 300 °C: Specific enthalpy of superheated steam = 3024.2 kJ/kg
At 2 MPa, 400 °C: Specific enthalpy of superheated steam = 3248.4 kJ/kg
At 1 kPa: Specific enthalpy of saturated water = 29.3 kJ/kg
At 1 kPa: Specific enthalpy of saturated vapour = 2513.7 kJ/kg
In the figures given below, L and H indicate low and high pressure centers, respectively; PGF, CoF and CeF indicate Pressure Gradient Force, Coriolis Force and Centrifugal Force, respectively; \( V \) is Velocity. [The arrows indicate only the directions but not the magnitudes of the forces and velocity.]
Which of the following is/are the correct representation(s) of the directions of various forces and velocity in the gradient wind balance in the northern hemisphere?
Which of the following is the correct form of the mass divergence form of the continuity equation for a compressible fluid? [In the given equations, \( \rho \) is the density and \( \nabla \) the three-dimensional velocity vector of the fluid.]
[(i)] $\displaystyle \frac{\partial \rho}{\partial t} + \nabla \times (\rho \mathbf{v}) = 0$
[(ii)] $\displaystyle \frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \mathbf{v}) = 0$
[(iii)] $\displaystyle \frac{\partial \mathbf{v}}{\partial t} + \rho \cdot \nabla \mathbf{v} = 0$
[(iv)] $\displaystyle \frac{\partial \rho}{\partial t} + \mathbf{v} \cdot \nabla \rho = 0$
The vertical (depth) profiles for three parameters P1, P2, and P3 in the northern Indian Ocean are given in the figure below. The values along the x-axis are the normalized values of the parameters and y-axis is the depth (m).
Identify the parameters P1, P2, and P3 from the options given below.