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author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
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committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /534/CH6/EX6.5/6_5_Heat_flux_Plate.sce | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '534/CH6/EX6.5/6_5_Heat_flux_Plate.sce')
-rw-r--r-- | 534/CH6/EX6.5/6_5_Heat_flux_Plate.sce | 24 |
1 files changed, 24 insertions, 0 deletions
diff --git a/534/CH6/EX6.5/6_5_Heat_flux_Plate.sce b/534/CH6/EX6.5/6_5_Heat_flux_Plate.sce new file mode 100644 index 000000000..4474214ba --- /dev/null +++ b/534/CH6/EX6.5/6_5_Heat_flux_Plate.sce @@ -0,0 +1,24 @@ +clear;
+clc;
+printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 6.5 Page 372 \n'); //Example 6.5
+// Heat Flux to blade when surface temp is reduced
+// Heat flux to a larger turbine blade
+
+//Operating Conditions
+v = 160; //[m/s] Velocity of air
+L = 0.04; //[m] Blade length
+Tsurr = 1150+273; //[K]
+Ts = 800+273; //[K] Surface Temp
+q = 95000; //[W/m^2] Original heat flux
+
+//Case 1
+Ts1 = 700+273; //[K] Surface Temp
+q1 = q*(Tsurr-Ts1)/(Tsurr-Ts);
+
+//Case 2
+L2 = .08; //[m] Length
+q2 = q*L/L2; //[W/m^2] Heat flux
+
+
+printf("\n\n (a) Heat Flux to blade when surface temp is reduced = %i KW/m^2 \n (b) Heat flux to a larger turbine blade = %.2f KW/m^2", q1/1000,q2/1000);
+//END
\ No newline at end of file |