Numerical investigation of the stall onset behaviour of the GA(W)-1 airfoil

DOI10.1016/S0045-7930(97)00052-2zbMath0974.76540OpenAlexW2068055129WikidataQ127570101 ScholiaQ127570101MaRDI QIDQ1974660

Max F. Platzer, Wolfgang Sanz

Publication date: 10 December 2001

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(97)00052-2

zbMATH Keywords

Reynolds-averaged Navier-Stokes equationsseparated flowalgebraic turbulence modelangles of attackGA(W)-1 airfoilmaximum lift coefficientnormal force fluctuationsone-equation turbulence modelstall onsetupwind-biased numerical scheme

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) (k)-(varepsilon) modeling in turbulence (76F60) General aerodynamics and subsonic flows (76G25)

Cites Work

• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
• Upwind Difference Schemes for Hyperbolic Systems of Conservation Laws

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