Step 1: The total hemispherical emissive power is defined as \[ E = \int_{\Omega = 2\pi} \int_{0}^{\infty} I_\lambda(\theta,\phi)\,\cos\theta \, d\Omega \, d\lambda, \] or, for a gray surface, \[ E = \varepsilon \sigma T^{4}. \] It is integrated over all directions and all wavelengths.
Step 2: Since the integration is over the full hemisphere, \(E\) is **not a function of the direction**. Therefore, statement (A) is true. Viewfactor pertains to radiative exchange between different surfaces, not to a single surface’s emissive power. Hence, statement (B) is false.
Step 3: Because \(E\) is integrated over wavelength/frequency, the **total hemispherical** \(E\) is not a function of wavelength or frequency variables themselves (though it depends on the spectral properties of the surface through the integral). Hence, statement (C) is false and statement (D) is true.
Final Answer: \[ \boxed{\;\; (A)\ \text{and}\ (D)\ \text{are true} \;} \]
An electrical wire of 2 mm diameter and 5 m length is insulated with a plastic layer of thickness 2 mm and thermal conductivity \( k = 0.1 \) W/(m·K). It is exposed to ambient air at 30°C. For a current of 5 A, the potential drop across the wire is 2 V. The air-side heat transfer coefficient is 20 W/(m²·K). Neglecting the thermal resistance of the wire, the steady-state temperature at the wire-insulation interface __________°C (rounded off to 1 decimal place).

GIVEN:
Kinematic viscosity: \( \nu = 1.0 \times 10^{-6} \, {m}^2/{s} \)
Prandtl number: \( {Pr} = 7.01 \)
Velocity boundary layer thickness: \[ \delta_H = \frac{4.91 x}{\sqrt{x \nu}} \]
The first-order irreversible liquid phase reaction \(A \to B\) occurs inside a constant volume \(V\) isothermal CSTR with the initial steady-state conditions shown in the figure. The gain, in kmol/m³·h, of the transfer function relating the reactor effluent \(A\) concentration \(c_A\) to the inlet flow rate \(F\) is:

A hot plate is placed in contact with a cold plate of a different thermal conductivity as shown in the figure. The initial temperature (at time $t = 0$) of the hot plate and cold plate are $T_h$ and $T_c$, respectively. Assume perfect contact between the plates. Which one of the following is an appropriate boundary condition at the surface $S$ for solving the unsteady state, one-dimensional heat conduction equations for the hot plate and cold plate for $t>0$?

The following data is given for a ternary \(ABC\) gas mixture at 12 MPa and 308 K:

\(y_i\): mole fraction of component \(i\) in the gas mixture
\(\hat{\phi}_i\): fugacity coefficient of component \(i\) in the gas mixture at 12 MPa and 308 K
The fugacity of the gas mixture is _________ MPa (rounded off to 3 decimal places).