Behaviour of a rectangular wing in a supersonic flow-dynamic pressure and normal force analysis in the range 1.3-4.0 mach

DOI10.1016/0045-7825(85)90077-5zbMATH Open0577.76008OpenAlexW2091550474MaRDI QIDQ1065639

O. M. Barturen, H. O. Quaranta, J. E. Eterovic

Publication date: 1985

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(85)90077-5

zbMATH Keywords

dynamic pressurecomputer-aided design of rocket wingsmeteorological rocketsrectangular wingtotal normal forces

Mathematics Subject Classification ID

Software, source code, etc. for problems pertaining to fluid mechanics (76-04) Basic methods in fluid mechanics (76M99)

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