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Pressure-Sensitive Paint Measurement of a Subsonic Diffuser Controlled by Sweeping Jets

扩散器(光学) 基督教牧师 中国 功率(物理) 工程教育 中华人民共和国 机械工程 物理 政治学 光学 工程类 法学 量子力学 光源
作者
Xin Wen,Jinsheng Song,Fan Yang,Di Peng,Yingzheng Liu
出处
期刊:AIAA Journal [American Institute of Aeronautics and Astronautics]
卷期号:60 (12): 6963-6970 被引量:1
标识
DOI:10.2514/1.j061885
摘要

No AccessTechnical NotesPressure-Sensitive Paint Measurement of a Subsonic Diffuser Controlled by Sweeping JetsXin Wen, Jinsheng Song, Fan Yang, Di Peng and Yingzheng LiuXin WenState Key Laboratory of Aerodynamics, 621000 Mianyang, People’s Republic of China*Associate Professor; also Key Laboratory of Education Ministry for Power Machinery and Engineering, School of Mechanical and Power Engineering, Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China.Search for more papers by this author, Jinsheng SongShanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China†Graduate Student, Key Laboratory of Education Ministry for Power Machinery and Engineering, School of Mechanical and Power Engineering.Search for more papers by this author, Fan YangShanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China†Graduate Student, Key Laboratory of Education Ministry for Power Machinery and Engineering, School of Mechanical and Power Engineering.Search for more papers by this author, Di PengShanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China‡Professor, Key Laboratory of Education Ministry for Power Machinery and Engineering, School of Mechanical and Power Engineering.Search for more papers by this author and Yingzheng LiuShanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China§Distinguished Professor, Key Laboratory of Education Ministry for Power Machinery and Engineering, School of Mechanical and Power Engineering; (Corresponding Author)Search for more papers by this authorPublished Online:22 Aug 2022https://doi.org/10.2514/1.J061885SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Collie W., Burgun R., Heinzen S., Hall C. and Chokani N., “Advanced Propulsion System Design and Integration for a Turbojet Powered Unmanned Aerial Vehicle,” AIAA Paper 2003-0415, 2003. https://doi.org/10.2514/6.2003-415 Google Scholar[2] Amici C., Ceresoli F., Pasetti M., Saponi M., Tiboni M. and Zanoni S., “Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles,” Applied Sciences, Vol. 11, No. 11, 2021, Paper 5209. https://doi.org/10.3390/app11115209 Google Scholar[3] Cherry E. 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Experiments in Fluids, Vol. 30, No. 3, 2001, pp. 262–272. https://doi.org/10.1007/s003480000172 Google Scholar[44] Burrows T. J., Vukasinovic B., Glezer A., Lakebrink M. T. and Mani M., “Experimental and Numerical Investigation of Active Flow Control of a Serpentine Diffuser,” AIAA Journal, Vol. 59, No. 1040, 2020, pp. 1–14. https://doi.org/10.2514/1.J059533 Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 60, Number 12December 2022 CrossmarkInformationCopyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. AcknowledgmentsThe authors gratefully acknowledge the financial support provided by the National Natural Science Foundation of China, China (Grant No. 12072196); the Science and Technology Commission of Shanghai Municipality, China (Grant No. 19JC1412900); the Advanced Jet Propulsion Innovation Center, China (AEAC HKCX2020-02-028); the Aeronautical Science Foundation of China (2020Z006057001); and the State Key Laboratory of Aerodynamics, China (SKLA-20200303).PDF Received27 March 2022Accepted25 July 2022Published online22 August 2022
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