Frequency response of positive-displacement variable-stroke fuel pump /
The dynamic characteristics of an axial-piston, variable-stroke jet-engine fuel pump were experimentally determined by frequency-response tests. It was found that the pump can be approximated by a first-order linear system with an average time constant of 0.04 second. The order of magnitude of the l...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1950
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2109 |
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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 2109 |
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