Transonic swept wings studied by the lifting-line theory

DOI10.2514/3.7837zbMath0471.76072OpenAlexW2020894349MaRDI QIDQ3926255

No author found.

Publication date: 1981

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/28fcdf7fdd5fad405942c47a05d734e4fa7209bc

zbMATH Keywords

relaxation methodswept wingsasymptotic perturbation analysisclassical non linear transonic small perturbation equationextensions of classical lifting line theoryhighly subcritical and shockless slightly supercritical flow regimesinner nearly two-dimensional regionline of vorticeslinear equation with known variable coefficientsMurman's fully conservative formouter fully three-dimensional domainPrandtl Glauert equationPrandtl's theory for high aspect ratio wingsthree-dimensional computer code FL022type sensitive difference operators

Mathematics Subject Classification ID

Transonic flows (76H05) Software, source code, etc. for problems pertaining to fluid mechanics (76-04) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (1)

Lifting-line theory of swept wings based on the full potential theory

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