Panel Aeroelastic Stability in Irregular Shock Reflection

气动弹性 空气动力学 颤振 航空学 工程类 物理 航空航天工程
作者
Yiwen He,Aiming Shi,Earl H. Dowell,Xiang Li
出处
期刊:AIAA Journal [American Institute of Aeronautics and Astronautics]
卷期号:60 (11): 6490-6499 被引量:10
标识
DOI:10.2514/1.j061902
摘要

No AccessTechnical NotesPanel Aeroelastic Stability in Irregular Shock ReflectionYiwen He, Aiming Shi, Earl H. Dowell and Xiang LiYiwen HeNorthwestern Polytechnical University, 710072 Xi'an, People's Republic of China, Aiming Shi https://orcid.org/0000-0002-1107-8925Northwestern Polytechnical University, 710072 Xi'an, People's Republic of China, Earl H. DowellDuke University, Durham, North Carolina 27708-0300 and Xiang LiNorthwestern Polytechnical University, 710072 Xi'an, People's Republic of ChinaPublished Online:17 Aug 2022https://doi.org/10.2514/1.J061902SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Dowell E. H., "Panel Flutter—A Review of the Aeroelastic Stability of Plates and Shells," AIAA Journal, Vol. 8, No. 3, 1970, pp. 385–399. https://doi.org/10.2514/3.5680 LinkGoogle Scholar[2] Dowell E. H., Aeroelasticity of Plates and Shells, Noordhoff International, Leyden, The Netherlands, 1975, pp. 1–9, Chap. 1. Google Scholar[3] Mei C., Abdel-Motagaly K. and Chen R., "Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds," Applied Mechanics Reviews, Vol. 52, No. 10, 1999, pp. 321–332. https://doi.org/10.1115/1.3098919 CrossrefGoogle Scholar[4] Shishaeva A., Vedeneev V., Aksenov A. and Sushko G., "Transonic Panel Flutter in Accelerating or Decelerating Flow Conditions," AIAA Journal, Vol. 56, No. 3, 2018, pp. 997–1010. https://doi.org/10.2514/1.J056217 LinkGoogle Scholar[5] Alder M., "Nonlinear Dynamics of Prestressed Panels in Low Supersonic Turbulent Flow," AIAA Journal, Vol. 54, No. 11, 2016, pp. 3632–3646. https://doi.org/10.2514/1.J054783 LinkGoogle Scholar[6] Visbal M., "On the Interaction of an Oblique Shock with a Flexible Panel," Journal of Fluids and Structures, Vol. 30, Feb. 2012, pp. 219–225. https://doi.org/10.1016/j.jfluidstructs.2012.02.002 CrossrefGoogle Scholar[7] Ye L.-Q. and Ye Z.-Y., "Effects of Shock Location on Aeroelastic Stability of Flexible Panel," AIAA Journal, Vol. 56, No. 9, 2018, pp. 3732–3744. https://doi.org/10.2514/1.J056924 LinkGoogle Scholar[8] Shi A., Chen J., Dowell E. H. and Wen H., "Approach to Determine the Most Efficient Supersonic Mach Number," AIAA Journal, Vol. 58, No. 3, 2020, pp. 1402–1406. https://doi.org/10.2514/1.J058773 LinkGoogle Scholar[9] Shi A., Chen J., Dowell E. H., Wen H., Li X. and Shen T., "Relativistic Oblique Shock: A Geometric Object," Astrophysical Journal, Vol. 893, No. 2, 2020, p. 167. https://doi.org/10.3847/1538-4357/ab7f28 CrossrefGoogle Scholar[10] Ben-Dor G., Shock Wave Reflection Phenomena, 2nd ed., Springer, Berlin, 2007, pp. 25–36, Chap. 1. Google Scholar[11] Visbal M., "Viscous and Inviscid Interactions of an Oblique Shock with a Flexible Panel," Journal of Fluids and Structures, Vol. 48, March 2014, pp. 27–45. https://doi.org/10.1016/j.jfluidstructs.2014.02.003 CrossrefGoogle Scholar[12] Dugundji J., Dowell E. and Perkin B., "Subsonic Flutter of Panels on Continuous Elastic Foundations," AIAA Journal, Vol. 1, No. 5, 1963, pp. 1146–1154. https://doi.org/10.2514/3.1738 LinkGoogle Scholar[13] Bisplinghoff R. L., Ashley H. and Halfman R. L., Aeroelasticity, Addison Wesley, Reading, MA, 1955, pp. 208–221, Chap. 5. Google Scholar[14] Anderson J., Fundamentals of Aerodynamics, 6th ed., McGraw–Hill, New York, 2017, pp. 626–630, Chap. 9. Google Scholar[15] Kornecki A., Dowell E. and O'Brien J., "On the Aeroelastic Instability of Two-Dimensional Panels in Uniform Incompressible Flow," Journal of Sound and Vibration, Vol. 47, No. 2, 1976, pp. 163–178. https://doi.org/10.1016/0022-460X(76)90715-X CrossrefGoogle Scholar[16] Stahara S. S. and Spreiter J. R., "Development of a Nonlinear Unsteady Transonic Flow Theory," NASA CR-2258, 1973. Google Scholar[17] Dowell E. H., A Modern Course in Aeroelasticity, 6th ed., Springer, Berlin, 2022, pp. 231–258, Chap. 4. Google Scholar[18] Bolotin V. V., "Dynamic Instabilities in Mechanics of Structures," Applied Mechanics Reviews, Vol. 52, No. 1, 1999, pp. R1–R9. https://doi.org/10.1115/1.3098924 Google Scholar[19] Reynolds R. R., "On the Nonlinear Aeroelasticity of Panels," Ph.D. Dissertation, Dept. of Mechanical Engineering and Materials Science, Duke Univ., Durham, NC, 1993. Google Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byAn Improved Model for Panel Aeroelastic Stability in Irregular Shock ReflectionYiwen He, Aiming Shi and Asghar Saba19 January 2023 What's Popular Volume 60, Number 11November 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. AcknowledgmentsThis work was supported by the Fundamental Research Funds for the Central Universities (grant no. D5000220189) and the Fund of NPU-Duke China Seed Program (grant no. 119003067), and partly by the project of the Ministry of Industry and Information Technology of China (grant no. CARP-2018F8-3). The authors are grateful for the valuable comments and suggestions from the editorial committee and anonymous referees. The authors also thank the journal production team for efficiently arranging the production process.PDF Received31 March 2022Accepted12 July 2022Published online17 August 2022
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