θ

Inclined & Horizontal Plate Natural Convection

Analyze natural convection boundary layers on flat plates oriented at arbitrary angles from vertical.

Gravity (g) Plate (Ts) Length L θ = 0°

Effective Gravity and Angle

For inclined plates ($\theta < 90^\circ$ from vertical), natural convection correlations are modified by replacing the standard gravity constant $g$ with the effective parallel component: $$g_{eff} = g \cos \theta$$ For horizontal plates ($\theta = 90^\circ$), fluid buoyancy forces form rising plumes (on upper hot/lower cold surfaces) or stable stratification layers (on lower hot/upper cold surfaces).

Parameters Setup

📐 Geometry & Orientation
🌡️ Temperatures
↔️ Boundary & Fluid

Results & Curves

5.936e+8
Rayleigh Ra
104.6523
Nusselt Nu
5.5047
h [W/m²K]
45.4139
Heat rate Q [W]

📈 Nusselt number vs Temperature difference (dT)

Engine Output

============================================
  INCLINED & HORIZONTAL PLATE CONVECTION
============================================

  Rayleigh Number Ra      =     5.9360E+08
  Nusselt Number Nu       =     104.6523
  Coeff h                 =       5.5047 W/m2K
  Transfer Q              =      45.4139 W

--- DELTA-T SWEEP ---
  dT[C]      Ra           Nu        h[W/m2K]   Q[W]
  ------------------------------------------------------------
      1.00   1.079E+07     31.897      1.6778        0.2517
      7.83   8.454E+07     58.088      3.0554        3.5901
     14.67   1.583E+08     70.065      3.6854        8.1079
     21.50   2.320E+08     78.626      4.1357       13.3377
     28.33   3.058E+08     85.482      4.4964       19.1096
     35.17   3.795E+08     91.287      4.8017       25.3289
     42.00   4.533E+08     96.366      5.0689       31.9338
     48.83   5.270E+08    100.910      5.3079       38.8801
     55.67   6.008E+08    105.039      5.5251       46.1344
     62.50   6.746E+08    108.837      5.7248       53.6702
     69.33   7.483E+08    112.362      5.9102       61.4664
     76.17   8.221E+08    115.658      6.0836       69.5051
     83.00   8.958E+08    118.759      6.2467       77.7714
     89.83   9.696E+08    121.690      6.4009       86.2523
     96.67   1.043E+09    124.474      6.5474       94.9366
    103.50   1.117E+09    127.128      6.6869      103.8145
    110.33   1.191E+09    129.665      6.8204      112.8771
    117.17   1.265E+09    132.097      6.9483      122.1167
    124.00   1.338E+09    134.435      7.0713      131.5261
    130.83   1.412E+09    136.687      7.1898      141.0990
    137.67   1.486E+09    138.861      7.3041      150.8296
    144.50   1.560E+09    140.963      7.4146      160.7124
    151.33   1.633E+09    142.998      7.5217      170.7427
    158.17   1.707E+09    144.972      7.6255      180.9157
    165.00   1.781E+09    146.889      7.7264      191.2274

Calculation Methodology

Mathematical Model & Theory

Natural convection on inclined flat plates is calculated using Churchill & Chu's vertical plate correlation with modified parallel gravity: $$g_{eff} = g \cos \theta$$ $$\text{Nu}_L = \left\{0.825 + \frac{0.387 \text{Ra}_L^{1/6}}{\left[1 + (0.492/\text{Pr})^{9/16}\right]^{8/27}}\right\}^2$$ For horizontal plates ($\theta = 90^\circ$), characteristic length is defined as: $$L_c = \frac{\text{Area}}{\text{Perimeter}} = \frac{L \cdot W}{2(L+W)}$$ Correlations for upper surface of hot plate / lower surface of cold plate: $$\text{Nu} = 0.54 \text{Ra}^{1/4} \quad (\text{Ra} < 10^7)$$ $$\text{Nu} = 0.15 \text{Ra}^{1/3} \quad (\text{Ra} \ge 10^7)$$ Correlations for lower surface of hot plate / upper surface of cold plate: $$\text{Nu} = 0.27 \text{Ra}^{1/4}$$

Academic References:

  1. Incropera, F. P., & DeWitt, D. P. (2011). Fundamentals of Heat and Mass Transfer. 7th Edition, John Wiley & Sons.
  2. Churchill, S. W., & Chu, H. S. (1975). Correlating Equations for Laminar and Turbulent Free Convection on a Vertical Plate. Int. J. Heat Mass Transfer.

Worked Engineering Example

Problem Statement:
A $0.5\text{ m} \times 0.3\text{ m}$ flat plate tilted at $30^\circ$ from vertical is maintained at $80^\circ\text{C}$ in ambient air at $25^\circ\text{C}$. Find the convection coefficient ($T_f = 52.5^\circ\text{C}$).

Step-by-step Solution:
1. Evaluate air properties at film temperature:
- $\nu = 1.83 \times 10^{-5}\text{ m}^2\text{/s}, \alpha = 2.6 \times 10^{-5}\text{ m}^2\text{/s}, k = 0.028\text{ W/m·K}, Pr = 0.71, \beta = 1/325.65 = 0.00307\text{ K}^{-1}$.
2. Calculate effective gravity:
$$g_{eff} = 9.81 \times \cos(30^\circ) = 8.495\text{ m/s}^2$$ 3. Compute Rayleigh number with $g_{eff}$ ($L_c = 0.5\text{ m}$):
$$\text{Ra}_L = \frac{g_{eff} \beta (T_s - T_a) L_c^3}{\nu \alpha} = \frac{8.495 \times 0.00307 \times (80-25) \times 0.5^3}{1.83 \times 10^{-5} \times 2.6 \times 10^{-5}} = 3.77 \times 10^8$$ 4. Compute Nusselt number using Churchill & Chu correlation:
$$\text{Nu}_L = \left\{0.825 + \frac{0.387 \times (3.77 \times 10^8)^{1/6}}{\left[1 + (0.492/0.71)^{9/16}\right]^{8/27}}\right\}^2 = \left\{0.825 + \frac{10.37}{1.157}\right\}^2 = 95.8$$ 5. Calculate convective coefficient $h$:
$$h = \frac{\text{Nu}_L k}{L_c} = \frac{95.8 \times 0.028}{0.5} = 5.36\text{ W/m}^2\text{K}$$