{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,5,4]],"date-time":"2026-05-04T13:46:47Z","timestamp":1777902407987,"version":"3.51.4"},"reference-count":21,"publisher":"SAGE Publications","issue":"6","license":[{"start":{"date-parts":[[2017,11,13]],"date-time":"2017-11-13T00:00:00Z","timestamp":1510531200000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/journals.sagepub.com\/page\/policies\/text-and-data-mining-license"}],"content-domain":{"domain":["journals.sagepub.com"],"crossmark-restriction":true},"short-container-title":["SIMULATION"],"published-print":{"date-parts":[[2018,6]]},"abstract":"<jats:p>Orthogonal design method is adopted to investigate the aerodynamic parameters simulation method of a canard guided rocket, in order to obtain one simulation method which can calculate the aerodynamic parameters quickly, reliably, and accurately. The turbulence model, mesh size, [Formula: see text]value and flow field size, which are regarded as the main factors in computational fluid dynamics (CFD) simulation, are divided into three levels for comparative analysis. Nine simulation combination schemes, which are representative and comprehensive, are singled out based on orthogonal table. The axial force coefficient and normal force coefficient in subsonic, transonic, and supersonic conditions are respectively calculated with these nine simulation combination schemes. The best simulation combination schemes in subsonic, transonic, and supersonic conditions are respectively picked out by intuitive analysis and synthesis balance analysis. The aerodynamic parameters in different velocities and attack angles, which were obtained by corresponding best simulation combination schemes, prove that the best simulation combination schemes are accurate. The results provide basis for the aerodynamic characteristic study of the canard guided rocket, and this research method can be used for the investigation on aerodynamic parameters simulation method of projectiles with different configurations.<\/jats:p>","DOI":"10.1177\/0037549717737854","type":"journal-article","created":{"date-parts":[[2017,11,13]],"date-time":"2017-11-13T10:49:06Z","timestamp":1510570146000},"page":"477-491","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":6,"title":["Investigation of the aerodynamic parameters simulation method of a guided rocket"],"prefix":"10.1177","volume":"94","author":[{"given":"Yong-Chao","family":"Chen","sequence":"first","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Xin-Bao","family":"Gao","sequence":"additional","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Min","family":"Gao","sequence":"additional","affiliation":[{"name":"Electronic Engineering Department, Shijiazhuang Mechanical Engineering College, Shijiazhuang, China"}],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"179","published-online":{"date-parts":[[2017,11,13]]},"reference":[{"key":"bibr1-0037549717737854","volume-title":"29th AIAA Applied Aerodynamic Conference","author":"Hamel N"},{"key":"bibr2-0037549717737854","volume-title":"26th International Symposium on Ballistics","author":"Je H"},{"issue":"5","key":"bibr3-0037549717737854","first-page":"157","volume":"27","author":"Fu B","year":"2006","journal-title":"Journal of Projectiles, Rockets, Missiles and Guidance"},{"key":"bibr4-0037549717737854","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2015.05.019"},{"key":"bibr5-0037549717737854","volume-title":"10th International Bhurban Conference on Applied Sciences & Technology","author":"Afzal S"},{"key":"bibr6-0037549717737854","volume-title":"Department of Defense - Proceedings of the HPCMP Users Group Conference 2006","author":"Sahu J."},{"issue":"6","key":"bibr7-0037549717737854","first-page":"596","volume":"32","author":"Xie Z-M","year":"2009","journal-title":"Journal of Solid Rocket Technology"},{"key":"bibr8-0037549717737854","volume-title":"2009 High Performance Computing Modernization Program users Group Conference","author":"Sahu J"},{"key":"bibr9-0037549717737854","doi-asserted-by":"publisher","DOI":"10.1108\/AEAT-03-2014-0030"},{"key":"bibr10-0037549717737854","doi-asserted-by":"publisher","DOI":"10.1080\/10618562.2013.867951"},{"key":"bibr11-0037549717737854","volume-title":"45th AIAA Aerospace Sciences Meeting and Exhibit","author":"Su W-J"},{"key":"bibr12-0037549717737854","volume-title":"37th National Conference on Theoretical and Mechanics","author":"Li C-C"},{"key":"bibr13-0037549717737854","first-page":"40","volume":"25","author":"Liu C","year":"2003","journal-title":"Journal of Detection & Control"},{"key":"bibr14-0037549717737854","unstructured":"Kun H, Zhenbei L. Project case of ANASYS ICEM CFD. Beijing, China: Post and Telecom Press, 2014, pp. 210\u2013212."},{"issue":"8","key":"bibr15-0037549717737854","first-page":"1049","volume":"31","author":"Hongli L","year":"2010","journal-title":"Acta Energiae Solaris Sinica"},{"key":"bibr16-0037549717737854","doi-asserted-by":"publisher","DOI":"10.1016\/S1001-6058(08)60095-5"},{"key":"bibr17-0037549717737854","unstructured":"Li Y, Hu C. Experiment design and date processing. 2015, pp. 178\u2013179. 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