Effect Of Diameter Of Closed End Coolant Passages On Natural Convection Water Cooling Of Gas Turbine Blades
Download Effect Of Diameter Of Closed End Coolant Passages On Natural Convection Water Cooling Of Gas Turbine Blades full books in PDF, epub, and Kindle. Read online free Effect Of Diameter Of Closed End Coolant Passages On Natural Convection Water Cooling Of Gas Turbine Blades ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
| Author | : Arthur N. Curren |
| Publisher | : |
| Total Pages | : 42 |
| Release | : 1956 |
| Genre | : Charts, diagrams, etc |
| ISBN | : |
An experimental investigation on a water-cooled gas turbine with blade coolant-passage diameters ranging from 0.100 to 0.500 inch, corresponding to length-to-diameter ratios of 25.5 to 5.1, in various quadrants of the turbine. The investigation was conducted to determine (1) whether coolant-passage length-to-ratio has a significant effect on natural-convection heat-transfer correlation, and (2) whether turbine blade temperatures could be calculated with reasonable accuracy from a theoretical natural-convection heat-transfer correlation.
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 208 |
| Release | : 1959 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 218 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 860 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 500 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Charles F. Zalabak |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1956 |
| Genre | : Aircraft gas-turbines |
| ISBN | : |
A water-cooled turbine was fabricated and tested to determine the effect of a connecting passage at the turbine rotor blade tip between a radial coolant passage 0.10 inch in diameter (length-diameter ratio = 25.5) and radial coolant passages in the legnth-diameter range of 5.1 to 20.4. Coolant flow through the connecting passage is induced by free-convection forces in the radial passages.
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 1300 |
| Release | : 1978 |
| Genre | : United States |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 2106 |
| Release | : 1959 |
| Genre | : Government publications |
| ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
| Author | : |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1979 |
| Genre | : |
| ISBN | : |
| Author | : G. James Van Fossen |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1979 |
| Genre | : Gas-turbines |
| ISBN | : |
