A study of the unsteady aerodynamics of a wing at high angles of attack using decambering to model separated flow

DOI10.1007/S12046-018-0894-YzbMath1398.76166OpenAlexW2810934654WikidataQ129647759 ScholiaQ129647759MaRDI QIDQ1615395

B. Antony Samuel, Rinku Mukherjee

Publication date: 31 October 2018

Published in: Sādhanā (Search for Journal in Brave)

Full work available at URL: https://www.ias.ac.in/describe/article/sadh/043/08/0121

zbMATH Keywords

separated flowwingaerodynamicsunsteadyhigh angle of attackdecamberingpost-stall

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Vortex methods applied to problems in fluid mechanics (76M23)

Cites Work

• Low-Speed Aerodynamics

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