Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine
Author : Jeffrey E. Haas
Publisher :
Page : 32 pages
File Size : 27,5 MB
Release : 1977
Category : Gas-turbines
ISBN :
Cold-air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine. 3: Effect of Rotor Tip Clearance on Overall Performance of a Solid Blade Configuration
Author : Jeffrey E. Haas
Publisher :
Page : 36 pages
File Size : 32,62 MB
Release : 1977
Category : Gas-turbines
ISBN :
Book Description
Two tip clearance configurations, one with a recess in the casing and the other with a reduced rotor blade height, were investigated at design equivalent speed over a range of tip clearance from about 2.0 to 5.0 percent of the stator blade height. The optimum configuration with a recess in the casing was the one where the rotor tip diameter was equal to the stator tip diameter (zero blade extension). For this configuration there was an approximate 1.5 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. For the reduced blade height configurations there was an approximate 2.0 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height.
Cold Air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine. 2: Effect of Air Ejection on Turbine Performance
Author :
Publisher :
Page : 46 pages
File Size : 46,12 MB
Release : 1977
Category :
ISBN :
Book Description
Cold-air Performance of Free Power Turbine Designed for 112-kilowatt Automotive Gas-turbine Engine 3: Effect of Stator Vane End Clearances on Performance
Author :
Publisher :
Page : 52 pages
File Size : 36,38 MB
Release : 1978
Category :
ISBN :
Book Description
NASA Technical Memorandum
Author :
Publisher :
Page : 56 pages
File Size : 48,23 MB
Release : 1978
Category : Aeronautics
ISBN :
Book Description
NASA Technical Paper
Author :
Publisher :
Page : 428 pages
File Size : 40,11 MB
Release : 1977
Category : Astronautics
ISBN :
Book Description
NASA Technical Paper
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 600 pages
File Size : 21,74 MB
Release : 1977
Category : Aeronautics
ISBN :
Book Description
Government Reports Annual Index
Author :
Publisher :
Page : 1610 pages
File Size : 43,14 MB
Release : 1978
Category : Research
ISBN :
Book Description
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.
NASA SP.
Author :
Publisher :
Page : 116 pages
File Size : 12,53 MB
Release : 1962
Category : Aeronautics
ISBN :
Book Description
Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 26 pages
File Size : 13,37 MB
Release : 2018-07-20
Category :
ISBN : 9781723249952
Book Description
Two tip clearance configurations, one with a recess in the casing and the other with a reduced rotor blade height, were investigated at design equivalent speed over a range of tip clearance from about 2.0 to 5.0 percent of the stator blade height. The optimum configuration with a recess in the casing was the one where the rotor tip diameter was equal to the stator tip diameter (zero blade extension). For this configuration there was an approximate 1.5 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. For the reduced blade height configurations there was an approximate 2.0 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. Haas, J. E. and Kofskey, M. G. Glenn Research Center NASA-TP-1032, E-9181 RTOP 505-04
