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Comparison Of Experimental And Analytical Aerodynamic Results For Blade With 12 Rows Of 0038 Centimeter 0015 In Diameter Coolant Holes Having Streamwise Ejection Angles
Download Comparison Of Experimental And Analytical Aerodynamic Results For Blade With 12 Rows Of 0038 Centimeter 0015 In Diameter Coolant Holes Having Streamwise Ejection Angles full books in PDF, epub, and Kindle. Read online Comparison Of Experimental And Analytical Aerodynamic Results For Blade With 12 Rows Of 0038 Centimeter 0015 In Diameter Coolant Holes Having Streamwise Ejection Angles ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723300318 Total Pages :24 pages Book Rating :4.3/5 (3 download)
Book Synopsis Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5 by : National Aeronautics and Space Administration (NASA)
Download or read book Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-20 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 multirow discharge covering coolant fractions from 0 to about 9 percent, the difference between the experimental and predicted results was no greater than about 1 percent in any case and less than 1/2 percent in most cases. Prust, H. W., Jr. Glenn Research Center NASA-TP-1204, E-9342 RTOP 505-04
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724754981 Total Pages :32 pages Book Rating :4.7/5 (549 download)
Book Synopsis Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 4 by : National Aeronautics and Space Administration (NASA)
Download or read book Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 4 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-06 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Previously published experimental aerodynamic efficiency results for a film cooled turbine stator blade are compared with analytical results computed from two published analytical methods. One method was used as published; the other was modified for certain cases of coolant discharge from the blade suction surface. For coolant ejection from blade surface regions where the surface static pressures are higher than the blade exit pressure, both methods predict the experimental results quite well. However, for ejection from regions with surface static pressures lower than the blade exit pressure, both methods predict too small a change in efficiency. The modified method gives the better prediction. Prust, H. W., Jr. Glenn Research Center NASA-TP-1151, E-9187 RTOP 505-04
