Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine
Author : Jeffrey E. Haas
Publisher :
Page : 32 pages
File Size : 22,77 MB
Release : 1977
Category : Gas-turbines
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Author : Jeffrey E. Haas
Publisher :
Page : 32 pages
File Size : 22,77 MB
Release : 1977
Category : Gas-turbines
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Author : Jeffrey E. Haas
Publisher :
Page : 28 pages
File Size : 42,15 MB
Release : 1975
Category : Axial flow
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A solid blade version of a single-stage, axial-flow turbine was investigated to determine its performance over a range of speeds from 0 to 105 percent of equivalent design speed and over a range of total to static pressure ratios from 1.62 to 5.07.
Author :
Publisher :
Page : 46 pages
File Size : 17,78 MB
Release : 1977
Category :
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Author :
Publisher :
Page : 540 pages
File Size : 22,31 MB
Release : 1977
Category : Astronautics
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Author : United States. National Aeronautics and Space Administration
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Page : 964 pages
File Size : 27,37 MB
Release : 1977
Category : Aeronautics
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Author :
Publisher :
Page : 326 pages
File Size : 50,91 MB
Release : 1975
Category :
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Author :
Publisher :
Page : 52 pages
File Size : 34,72 MB
Release : 1978
Category :
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Author :
Publisher :
Page : 56 pages
File Size : 48,48 MB
Release : 1978
Category : Aeronautics
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Author : Technology Reports Centre (Great Britain)
Publisher :
Page : 460 pages
File Size : 49,53 MB
Release : 1978
Category :
ISBN :
Author :
Publisher :
Page : 1610 pages
File Size : 23,95 MB
Release : 1978
Category : Research
ISBN :
Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.