Attainable circulation of airfoils in cascade /
From consideration of available information on boundary-layer behaviour, a relation among profile thickness, maximum surface velocity, Reynolds number, velocity diagram, and solidity is established for a cascade of airfoils immersed in a two-dimensional incompressible fluid flow. Several cascades ar...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1949
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1941 |
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 1941 |
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