Prediction of loaded airfoil unsteady aerodynamic gust response by a locally analytical method

DOI10.1016/0895-7177(88)90023-4zbMath0652.76040OpenAlexW2089677692MaRDI QIDQ1107388

H.-W. D. Chiang, Sanford Fleeter

Publication date: 1988

Published in: Mathematical and Computer Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0895-7177(88)90023-4

zbMATH Keywords

Analytical solutionsairfoil at finite nonzero angle of attackairfoil geometrybody-fitted computational gridcomplete first-order modeldiscrete algebraic equationsincompressible unsteady aerodynamicsindividual grid elementslocally analytical solutionsteady mean flowtransformed flow equationstwo-dimensional gust

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Basic methods in fluid mechanics (76M99)

Cites Work

• TOMCAT - a code for numerical generation of boundary-fitted curvilinear coordinate systems on fields containing any number of arbitrary two- dimensional bodies
• A complete second-order theory for the unsteady flow about an airfoil due to a periodic gust
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