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i n! GAS TURBINE APPLICATIONS by Ruymond s. CoUuduy ANALYSIS AND COMPARISON OF WALL COOLING SCHEMES FOR ADVANCED

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Figure

Figure 2.  - Offset rectangular plate fin configuration.
Figure 3.  - F l w  chart describing program logic.
Figure 5.  -Interaction  of convection and film  cooling.
Figure  7.  - Counterflow film-cooled  wall section.  Offset-plate-finned  cooling passage;  effective gas temperature,  2200 K  (3500'  F);  coolant  supply temperature,  811 K  (lOOOo  F)
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