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. M., Elkins C. J. and Eaton J. K., “Geometric Sensitivity of Three-Dimensional Separated Flows,” International Journal of Heat and Fluid Flow, Vol. 29, No. 3, 2008, pp. 803–811. https://doi.org/10.1016/j.ijheatfluidflow.2008.01.018 CrossrefGoogle Scholar[4] Ohlsson J., Schlatter P., Fischer P. F. and Henningson D. S., “Direct Numerical Simulation of Separated Flow in a Three-Dimensional Diffuser,” Journal of Fluid Mechanics, Vol. 650, May 2010, p. 307. https://doi.org/10.1017/S0022112010000558 CrossrefGoogle Scholar[5] Gil-Prieto D., MacManus D. G., Zachos P. K. and Bautista A., “Assessment Methods for Unsteady Flow Distortion in Aero-Engine Intakes,” Aerospace Science and Technology, Vol. 72, Jan. 2017, pp. 92–304. https://doi.org/10.1016/j.ast.2017.10.029 Google Scholar[6] Zachos P. K., MacManus D. G., Prieto D. G. and Chiereghin N., “Flow Distortion Measurements in Convoluted Aeroengine Intakes,” AIAA Journal, Vol. 54, No. 9, 2016, pp. 1–14. https://doi.org/10.2514/1.J054904 Google Scholar[7] Zhang B. F., Liu K., Zhou Y., To S. and Tu J. Y., “Active Drag Reduction of a High-Drag Ahmed Body Based on Steady Blowing,” Journal of Fluid Mechanics, Vol. 856, Dec. 2018, pp. 351–396. https://doi.org/10.1017/jfm.2018.703 CrossrefGoogle Scholar[8] Xu Y., Feng L. H. and Wang J. J., “Experimental Investigation of a Synthetic Jet Impinging on a Fixed Wall,” Experiments in Fluids, Vol. 54, No. 5, 2013, Paper 1512. https://doi.org/10.1007/s00348-013-1512-8 Google Scholar[9] Wang J. J., Choi K. S., Feng L. H., Jukes T. N. and Whalley R. D., “Recent Developments in DBD Plasma Flow Control,” Progress in Aerospace Sciences, Vol. 62, Oct. 2013, pp. 52–78. https://doi.org/10.1016/j.paerosci.2013.05.003 CrossrefGoogle Scholar[10] Corke T. C., Enloe C. L. and Wilkinson S. P., “Dielectric Barrier Discharge Plasma Actuators for Flow Control,” Annual Review of Fluid Mechanics, Vol. 42, No. 1, 2010, pp. 505–529. https://doi.org/10.1146/annurev-fluid-121108-145550 CrossrefGoogle Scholar[11] Gartner J., Rice T. T. and Amitay M., “Mitigation of Massively Separated Flow in a Three-Dimensional Diffuser,” International Journal of Heat and Fluid Flow, Vol. 76, April 2019, pp. 242–258. https://doi.org/10.1016/j.ijheatfluidflow.2019.01.015 CrossrefGoogle Scholar[12] Burrows T. J., Vukasinovic B. and Glezer A., “Fluidic Control of an Aggressive Offset Diffuser for a Supersonic Inlet,” AIAA Paper 2017-4304, 2017. https://doi.org/10.2514/6.2017-4304 Google Scholar[13] Ostermann F., Woszidlo R., Nayeri C. N. and Paschereit C. O., “Properties of a Sweeping Jet Emitted from a Fluidic Oscillator,” Journal of Fluid Mechanics, Vol. 857, Dec. 2018, pp. 216–238. https://doi.org/10.1017/jfm.2018.739 CrossrefGoogle Scholar[14] Woszidlo R., Ostermann F. and Schmidt H. J., “Fundamental Properties of Fluidic Oscillators for Flow Control Applications,” AIAA Journal, Vol. 57, No. 3, 2019, pp. 978–992. https://doi.org/10.2514/1.J056775 LinkGoogle Scholar[15] Tomac M. N., “Novel Jet Impingement Atomization by Synchronizing the Sweeping Motion of the Fluidic Oscillators,” Journal of Visualization, Vol. 23, No. 3, 2020, pp. 373–375. https://doi.org/10.1007/s12650-020-00632-3 CrossrefGoogle Scholar[16] Lin J. C., Whalen E. A., Andino M. Y., Graff E. C., Lacy D. S., Washburn A. E., Gharib M. and Wygnanski I. J., “Full-Scale Testing of Active Flow Control Applied to a Vertical Tail,” Journal of Aircraft, Vol. 56, Feb. 2019, pp. 1–11. https://doi.org/10.2514/1.C034907 Google Scholar[17] Dandois J., Verbeke C. and Ternoy F., “Performance Enhancement of a Vertical Tail Model with Sweeping Jets,” AIAA Journal, Vol. 58, Oct. 2020, pp. 1–14. https://doi.org/10.2514/1.J059161 Google Scholar[18] Koklu M. and Owens L. R., “Comparison of Sweeping Jet Actuators with Different Flow-Control Techniques for Flow-Separation Control,” AIAA Journal, Vol. 55, No. 3, 2017, pp. 848–860. https://doi.org/10.2514/1.J055286 LinkGoogle Scholar[19] Otto C., Tewes P., Little J. C. and Woszidlo R., “Comparison Between Fluidic Oscillators and Steady Jets for Separation Control,” AIAA Journal, Vol. 57, No. 12, 2019, pp. 5220–5229. https://doi.org/10.2514/1.J058081 LinkGoogle Scholar[20] Ebert C., Mihalyovics J., Staats M., Peitsch D. and Weiss J., “Numerical and Experimental Investigations for Super Sonic Active Flow Control in the Transsonic Mach Regime,” Conference: Deutscher Luft- und Raumfahrtkongress 2019, 2020, Paper 490165. https://doi.org/10.25967/490165 Google Scholar[21] Westerweel J., Elsinga G. E. and Adrian R. J., “Particle Image Velocimetry for Complex and Turbulent Flows,” Annual Review of Fluid Mechanics, Vol. 45, No. 1, 2013, pp. 409–436. https://doi.org/10.1146/annurev-fluid-120710-101204 CrossrefGoogle Scholar[22] Lee T., Lee C., Nonomura T. and Asai K., “Unsteady Skin-Friction Field Estimation Based on Global Luminescent Oil-Film Image Analysis,” Journal of Visualization, Vol. 23, No. 5, 2020, pp. 763–772. https://doi.org/10.1007/s12650-020-00661-y CrossrefGoogle Scholar[23] Liu T., Sullivan J. P., Asai K., Klein C. and Egami Y., Pressure and Temperature Sensitive Paints, Springer, Cham, 2021, pp. 3–7. https://doi.org/10.1007/978-3-030-68056-5 Google Scholar[24] Sugioka Y., Hiura K., Chen L., Matsui A., Morita K., Nonomura T. and Asai K., “Unsteady Pressure-Sensitive-Paint (PSP) Measurement in Low-Speed Flow: Characteristic Mode Decomposition and Noise Floor Analysis,” Experiments in Fluids, Vol. 60, No. 7, 2019, p. 108. https://doi.org/10.1007/s00348-019-2755-9 CrossrefGoogle Scholar[25] Gregory J. W., Asai K., Kameda M., Liu T. and Sullivan J. P., “A Review of Pressure-Sensitive Paint for High-Speed and Unsteady Aerodynamics,” Proceedings of the Institution of Mechanical Engineers Part G—Journal of Aerospace Engineering, Vol. 222, No. 2, 2008, pp. 249–290. https://doi.org/10.1243/09544100JAERO243 CrossrefGoogle Scholar[26] Gregory J. W., Sakaue H., Liu T. and Sullivan J. P., “Fast Pressure-Sensitive Paint for Flow and Acoustic Diagnostics,” Annual Review of Fluid Mechanics, Vol. 46, No. 1, 2014, pp. 303–330. https://doi.org/10.1146/annurev-fluid-010313-141304 CrossrefGoogle Scholar[27] Peng D. and Liu Y., “Fast Pressure-Sensitive Paint for Understanding Complex Flows: From Regular to Harsh Environments,” Experiments in Fluids, Vol. 61, No. 1, 2019, Paper 8. https://doi.org/10.1007/s00348-019-2839-6 Google Scholar[28] Tagliabue A., Scharnowski S. and Kähler C. J., “Surface Pressure Determination: A Comparison Between PIV-Based Methods and PSP Measurements,” Journal of Visualization, Vol. 20, No. 3, 2017, pp. 581–590. https://doi.org/10.1007/s12650-016-0406-2 CrossrefGoogle Scholar[29] Flaherty W., Reedy T. M., Elliott G. S., Austin J. M., Schmit R. F. and Crafton J., “Investigation of Cavity Flow Using Fast-Response Pressure Sensitive Paint,” 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-0678, Jan. 2013. https://doi.org/10.2514/6.2013-678 Google Scholar[30] Huang C. Y., Hu Y. H., Wan S. A. and Nagai H., “Application of Pressure-Sensitive Paint for the Characterization of Mixing with Various Gases in T-Type Micromixers,” International Journal of Heat and Mass Transfer, Vol. 156, Aug. 2020, Paper 119710. https://doi.org/10.1016/j.ijheatmasstransfer.2020.119710 Google Scholar[31] Gardner A. D., Klein C., Sachs W. E., Henne U., Mai H. and Richter K., “Investigation of Three-Dimensional Dynamic Stall on an Airfoil Using Fast-Response Pressure-Sensitive Paint,” Experiments in Fluids, Vol. 55, Aug. 2014, Paper 1807. https://doi.org/10.1007/s00348-014-1807-4 Google Scholar[32] Jiao L., Chen Y., Wen X., Peng D., Liu Y. and Gregory J. W., “Resolving Vortex-Induced Pressure Fluctuations on a Cylinder in Rotor Wake Using Fast-Responding Pressure-Sensitive Paint,” Physics of Fluids, Vol. 31, No. 5, 2019, Paper 055106. https://doi.org/10.1063/1.5092944 Google Scholar[33] Peng D., Xie F., Liu X., Lin J., Li Y., Zhong J., Zhang Q. and Liu Y., “Experimental Study on Hypersonic Shock–Body Interaction Between Bodies in Close Proximity Using Translucent Fast Pressure- and Temperature-Sensitive Paints,” Experiments in Fluids, Vol. 61, No. 5, 2020, Paper 120. https://doi.org/10.1007/s00348-020-02948-0 Google Scholar[34] Gößling J., Ahlefeldt T. and Hilfer M., “Experimental Validation of Unsteady Pressure-Sensitive Paint for Acoustic Applications,” Experimental Thermal and Fluid Science, Vol. 112, April 2019, Paper 109915. https://doi.org/10.1016/j.expthermflusci.2019.109915 Google Scholar[35] Burrows T. J., Vukasinovic B. and Glezer A., “Control of a Transonic Shock in a Serpentine Diffuser Using Surface Fluidic Actuation,” AIAA Aviation 2019 Forum, AIAA Paper 2019-3687, 2019. https://doi.org/10.2514/6.2019-3687 LinkGoogle Scholar[36] Burrows T. J., Vukasinovic B. and Glezer A., “Active Control of a 3-D Flow Separation Induced by a Transonic Shock,” Experiments in Fluids, Vol. 62, No. 9, 2021, Paper 187. https://doi.org/10.1007/s00348-021-03280-x Google Scholar[37] Gartner J. and Amitay M., “Flow Control in a Diffuser at Transonic Conditions,” 45th AIAA Fluid Dynamics Conference, AIAA Paper 2015-2484, 2015. https://doi.org/10.2514/6.2015-2484 LinkGoogle Scholar[38] Li Z., Liu J., Zhou W., Liu Y. and Wen X., “Experimental Investigation of Flow Dynamics of Sweeping Jets Impinging Upon Confined Concave Surfaces,” International Journal of Heat and Mass Transfer, Vol. 142, Oct. 2019, Paper 118457. https://doi.org/10.1016/j.ijheatmasstransfer.2019.118457 Google Scholar[39] Koklu M. and Melton L. M., “Sweeping Jet Actuator in a Quiescent Environment,” 43rd AIAA Fluid Dynamics Conference, AIAA Paper 2013-2477, 2013. https://doi.org/10.2514/6.2013-2477 LinkGoogle Scholar[40] Woszidlo R. and Little J. C., “Recommended Practices for Characterization and Documentation of Active Flow Control Actuators,” AIAA Scitech 2021 Forum, AIAA Paper 2021-2002, 2021. https://doi.org/10.2514/6.2021-2002 LinkGoogle Scholar[41] Peng D., Gu F., Li Y. and Liu Y., “A Novel Sprayable Fast-Responding Pressure-Sensitive Paint Based on Mesoporous Silicone Dioxide Particles,” Sensors and Actuators A Physical, Vol. 279, Aug. 2018, pp. 390–398. https://doi.org/10.1016/j.sna.2018.06.048 CrossrefGoogle Scholar[42] Crafton J. W., Gregory J., Sellers M. and Ruyten W., “Data Processing Tools for Dynamic Pressure-Sensitive Paint,” 55th AIAA Aerospace Sciences Meeting, AIAA Paper 2017-0701, 2017. https://doi.org/10.2514/6.2017-0701 LinkGoogle Scholar[43] Lee I. and Sung H. J., “Characteristics of Wall Pressure Fluctuations in Separated and Reattaching Flows over a Backward-Facing Step: Part 1,” Time-Mean Statistics and Cross-Spectral Analyses. 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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