naca-report-1220
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- November 2, 2016 Create Date
- November 2, 2016 Last Updated
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National Advisory Committee for Aeronautics, Report - Calculations of Laminar Heat Transfer around Cylinders of Arbitrary Cross Section and Transpiration Cooled Walls with Application to Turbine Blade Cooling
| File | Action |
|---|---|
| naca-report-1220 Calculations of Laminar Heat Transfer around Cylinders of Arbitrary Cross Section and Transpiration Cooled Walls with Application to Turbine Blade Cooling.pdf | Download |
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