Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine
Author : Jeffrey E. Haas
Publisher :
Page : 32 pages
File Size : 15,58 MB
Release : 1977
Category : Gas-turbines
ISBN :
Author : Jeffrey E. Haas
Publisher :
Page : 32 pages
File Size : 15,58 MB
Release : 1977
Category : Gas-turbines
ISBN :
Author : Jeffrey E. Haas
Publisher :
Page : 28 pages
File Size : 11,48 MB
Release : 1975
Category : Axial flow
ISBN :
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 : 11,35 MB
Release : 1977
Category :
ISBN :
Author : Jeffrey E. Haas
Publisher :
Page : 44 pages
File Size : 28,92 MB
Release : 1977
Category : Aerodynamics
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Author :
Publisher :
Page : 326 pages
File Size : 26,7 MB
Release : 1975
Category :
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Author :
Publisher :
Page : 52 pages
File Size : 12,89 MB
Release : 1978
Category :
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Author :
Publisher :
Page : 540 pages
File Size : 21,10 MB
Release : 1977
Category : Astronautics
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Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 964 pages
File Size : 23,12 MB
Release : 1977
Category : Aeronautics
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Author :
Publisher :
Page : 56 pages
File Size : 11,79 MB
Release : 1978
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 330 pages
File Size : 29,24 MB
Release : 1978
Category : Aeronautics
ISBN :