The influence of airfoil thickness and Reynolds number on separation

DOI10.1007/BF00944968zbMath0504.76042OpenAlexW1970437816MaRDI QIDQ1836366

Yanyan Li

Publication date: 1982

Published in: ZAMP. Zeitschrift für angewandte Mathematik und Physik (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00944968

zbMATH Keywords

bifurcationnonuniquenessKirchhoff theoryReynolds numbersattached motion past finite flat platebody thickness increasesfree steamline inviscid approachlaminar symmetric flowseparated motion past a bluff bodytrailing and leading edgesviscous triple- deck requirementwake dimensions and drag abruptly increase

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Wakes and jets (76D25)

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Cites Work

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