Development of a smart nozzle
This work is currently at a very preliminary stage. The performance test of the nozzle was limited at low Mach numbers and low frequencies, due to several facts, including the low speed of the control hardware. Further studies will obviously be necessary to improve the control system and to extend t...
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sg-ntu-dr.10356-68882023-03-04T18:08:32Z Development of a smart nozzle Huang, Xiaoyang. School of Mechanical and Production Engineering DRNTU::Engineering::Manufacturing This work is currently at a very preliminary stage. The performance test of the nozzle was limited at low Mach numbers and low frequencies, due to several facts, including the low speed of the control hardware. Further studies will obviously be necessary to improve the control system and to extend the test to high speed jet flows, e.g., supersonic jets, where screech tones may occur. 2008-09-17T14:36:21Z 2008-09-17T14:36:21Z 1999 1999 Research Report http://hdl.handle.net/10356/6888 Nanyang Technological University application/pdf |
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DRNTU::Engineering::Manufacturing Huang, Xiaoyang. Development of a smart nozzle |
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This work is currently at a very preliminary stage. The performance test of the nozzle was limited at low Mach numbers and low frequencies, due to several facts, including the low speed of the control hardware. Further studies will obviously be necessary to improve the control system and to extend the test to high speed jet flows, e.g., supersonic jets, where screech tones may occur. |
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School of Mechanical and Production Engineering |
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School of Mechanical and Production Engineering Huang, Xiaoyang. |
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Research Report |
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Huang, Xiaoyang. |
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Huang, Xiaoyang. |
title |
Development of a smart nozzle |
title_short |
Development of a smart nozzle |
title_full |
Development of a smart nozzle |
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Development of a smart nozzle |
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Development of a smart nozzle |
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development of a smart nozzle |
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2008 |
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http://hdl.handle.net/10356/6888 |
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