Mon Nov 12 07:28:06 EST 2007
Input file [ flatplate.txt ]
#----------------------Input---------------------#
Length		200.		(mm) 	
Velocity	50.		(m/s) 	
Rgas		.287		(units)	
kgas		.02626		(W/m/k) 	
Cpgas		1.004		(kJ/kg/degK) 	
mugas		.00001813	(kg/m/s) 	
Tflow		27.		(deg C) 	
Pflow		101.0		(kPa) 	
Turb		.01		(non-dim) 	
#----------------------Output--------------------#
Gas Density         1.172
Prandlt No.         0.693
Reyn(L)            646701
Re(crit)         453579.9
Xcrit(mm)           140.3
Avg. h               99.3
 
tlbt(mm) is the thermal boundary layer thickness in mm's
Turbulent BL thickness > laminar BL thickness, however
HTC(turbulent) is still >> HTC(laminar)
 
   X(mm)     Ren(x) tblt(mm)     Hlam    Hturb     H(x) 
   10.00      32335     0.31      139      279      139 ##################
   20.00      64670     0.44       98      243       98 #############
   30.00      97005     0.53       80      224       80 ##########
   40.00     129340     0.62       69      211       69 #########
   50.00     161675     0.69       62      202       62 ########
   60.00     194010     0.75       57      195       57 #######
   70.00     226345     0.82       52      189       52 #######
   80.00     258680     0.87       49      184       49 #######
   90.00     291015     0.92       46      180       46 ######
  100.00     323350     0.97       44      176       44 ######
  110.00     355685     1.02       42      173       42 ######
  120.00     388020     1.07       40      170       40 #####
  130.00     420355     1.11       38      167       38 #####
  140.00     452690     1.15       37      164       37 #####
  150.00     485026     4.69       36      162      162 #####################
  160.00     517361     4.94       35      160      160 ####################
  170.00     549696     5.18       34      158      158 ####################
  180.00     582031     5.43       33      156      156 ####################
  190.00     614366     5.67       32      155      155 ####################
  200.00     646701     5.90       31      153      153 ###################
#.......................End of File..............#