Method of analysis for compressible flow past arbitrary turbomachine blades on general surface of revolution / Chung-Hua Wu and Curtis A. Brown.
A method of obtaining the flow of a nonviscous compressible fluid past compressor and turbine blades on a general surface of revolution by the use of differentiation coefficients for unequally spaced grid points is given. Solutions by the relaxation method for hand computation and the matrix method...
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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) ;
2407. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2407
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| Y 3.N 21/5:6/2407 | Available Place a Hold |