Read Online Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Blade with 12 Rows of 0.038-Centimeter-(0.015 Inch) Diameter Coolant Holes Having Streamwise Ejection Angles - National Aeronautics and Space Administration file in ePub Online

Read Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Blade with 12 Rows of 0.038-Centimeter-(0.015 Inch) Diameter Coolant Holes Having Streamwise Ejection Angles - National Aeronautics and Space Administration | ePub

Published experimental aerodynamic efficiency results were compared with results predicted from two published analytical methods. This is the second of two such comparisons. One of the analytical methods was used as published; the other was modified for certain cases of coolant discharge from the blade suction surface. The results show that for 23 cases of single row and

Title : Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Blade with 12 Rows of 0.038-Centimeter-(0.015 Inch) Diameter Coolant Holes Having Streamwise Ejection Angles
Author : National Aeronautics and Space Administration
Language : en
Rating :
4.90 out of 5 stars
Type : PDF, ePub, Kindle
Uploaded : Apr 07, 2021

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