Interference method for obtaining the potential flow past an arbitrary cascade of airfoils /
A procedure is presented for obtaining the pressure distribution in a two-dimensional, incompressible, and nonviscous flow on an arbitrary airfoil section in cascade. The method consides directly the influence on a given airfoil of the rest of the cascade and evaluates this interference by an iterat...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1947
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1252 |
| Subjects: |
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 1252 |
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