Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines / John T. Sinnette, Jr., and George R. Costello.
A theoretical discussion of the application of blade boundary-layer control to increase the efficiency and the stage pressure ratio and to improve off-design performance of compressors and turbines is presented. A method based on the potentioal flow a compressible fluid is developed for designing su...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2371. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2371
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| Y 3.N 21/5:6/2371 | Available Place a Hold |