The performance of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with cast airfoil-shaped and bent sheet-metal nozzle blades / by David S. Gabriel and L. Robert Carman.
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| Corporate Authors: | , |
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| Other title: | NACA Wartime Reports. Series E. Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. E233. |
| Subjects: |
| Abstract: | Efficiency tests have been made on a single-stage gas turbine having an 11.0-inch pitch-line diameter wheel and a nozzle diaphragm with cast airfoil-shaped nozzle blades using atmospheric air as the driving fluid. A comparison of these tests with previous tests made on the same turbine but with a nozzle diaphragm having fabricated bent sheet-metal blades is given. |
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| Item Description: | NACA Wartime Report E-233. Originally issued as NACA as Advance Restricted Report E5H31 (September 1945) Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio. |
| Physical Description: | 5 pages, 5 unnumbered pages : illustrations ; 27 cm. |
| Bibliography: | Includes bibliographical references. |
| Action Note: | will digitize 20150604 Queued for digitization June 4, 2015 |