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 = 90°

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

7.108e+8
Rayleigh Ra
44.0856
Nusselt Nu
288.2611
h [W/m²K]
2378.1545
Heat rate Q [W]

📈 Nusselt number vs Temperature difference (dT)

Engine Output

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

  Rayleigh Number Ra      =     7.1078E+08
  Nusselt Number Nu       =      44.0856
  Coeff h                 =     288.2611 W/m2K
  Transfer Q              =    2378.1545 W

--- DELTA-T SWEEP ---
  dT[C]      Ra           Nu        h[W/m2K]   Q[W]
  ------------------------------------------------------------
      1.00   1.292E+07     16.188    105.8511       15.8777
      7.83   1.012E+08     27.083    177.0851      208.0750
     14.67   1.895E+08     31.680    207.1468      455.7230
     21.50   2.778E+08     34.859    227.9319      735.0803
     28.33   3.662E+08     37.349    244.2136     1037.9078
     35.17   4.545E+08     39.422    257.7675     1359.7238
     42.00   5.428E+08     41.212    269.4684     1697.6506
     48.83   6.311E+08     42.794    279.8173     2049.6616
     55.67   7.194E+08     44.219    289.1307     2414.2416
     62.50   8.077E+08     45.517    297.6223     2790.2089
     69.33   8.960E+08     46.713    305.4436     3176.6129
     76.17   9.843E+08     47.824    312.7063     3572.6699
     83.00   1.073E+09     48.863    319.4957     3977.7210
     89.83   1.161E+09     49.839    325.8778     4391.2038
     96.67   1.249E+09     50.760    331.9056     4812.6317
    103.50   1.338E+09     51.635    337.6218     5241.5790
    110.33   1.426E+09     52.467    343.0616     5677.6697
    117.17   1.514E+09     53.261    348.2543     6120.5689
    124.00   1.602E+09     54.021    353.2245     6569.9764
    130.83   1.691E+09     54.750    357.9934     7025.6208
    137.67   1.779E+09     55.452    362.5790     7487.2562
    144.50   1.867E+09     56.127    366.9969     7954.6579
    151.33   1.956E+09     56.779    371.2608     8427.6201
    158.17   2.044E+09     57.410    375.3826     8905.9531
    165.00   2.132E+09     58.020    379.3730     9389.4819

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 $h$:
$$h = \frac{\text{Nu}_L k}{L_c} = \frac{95.8 \times 0.028}{0.5} = 5.36\text{ W/m}^2\text{K}$$