The design of shock-free supercritical airfoils including viscous effects

DOI10.1002/CNM.1630020107zbMath0604.76043OpenAlexW1978592607MaRDI QIDQ3741284

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Publication date: 1986

Published in: Communications in Applied Numerical Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/cnm.1630020107

zbMATH Keywords

boundary layernumerical procedureiterative processconformal mapviscous effectstransition modelinviscid solutiontransition to turbulent flowCrank-Nicolson type implicit finite difference schemedisplacement surface conceptfull stream functioninverse-boundary layer algorithminviscid hodograph-based inverse-design algorithmLevy-Lees variablesnumerical coupling procedureshock-free supercritical airfoil sectionsturbulent boundary layer equationstwo-sheeted hodograph plane

Mathematics Subject Classification ID

Transonic flows (76H05) General aerodynamics and subsonic flows (76G25) Turbulence (76F99) Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

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