Aircraft performance obtained from modified point mass model

Abstract

ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und MechanikVolume 81, Issue S3 p. 625-626 Article Aircraft performance obtained from modified point mass model M. Vrdoljak, M. Vrdoljak mvrdolja@jagor.srce.hr Institute for Defense Studies, Research and Development, p.p.252, HR-10002 Zagreb, CroatiaSearch for more papers by this authorS. Jankovic, S. Jankovic slobodan.jankovic@zg.tel.hr Department of Aerospace, Faculty of Mechanical Engineering and Naval Architecture, I. LuČICA 5, HR-10000 Zagreb, CroatiaSearch for more papers by this author M. Vrdoljak, M. Vrdoljak mvrdolja@jagor.srce.hr Institute for Defense Studies, Research and Development, p.p.252, HR-10002 Zagreb, CroatiaSearch for more papers by this authorS. Jankovic, S. Jankovic slobodan.jankovic@zg.tel.hr Department of Aerospace, Faculty of Mechanical Engineering and Naval Architecture, I. LuČICA 5, HR-10000 Zagreb, CroatiaSearch for more papers by this author First published: 18 March 2011 https://doi.org/10.1002/zamm.20010811589Citations: 1AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onFacebookTwitterLinkedInRedditWechat No abstract is available for this article.Citing Literature Volume81, IssueS3Supplement: Short Communications in Mathematics and Mechanics Section 9-29, University of Göttingen, Germany April 2-7, 20002001Pages 625-626 RelatedInformation