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Anderson, 2003 - Google Patents

Non-intrusive sensing and feedback control of serpentine inlet flow distortion

Anderson, 2003

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Document ID
11087892336946355683
Author
Anderson J
Publication year

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A technique to infer circumferential total pressure distortion intensity found in serpentine inlet airflow was established using wall-pressure fluctuation measurements. This sensing technique was experimentally developed for aircraft with serpentine inlets in a symmetric …
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