Redesign of a supercritical wing in the presence of an engine nacelle

DOI10.1016/0021-9991(87)90135-5zbMath0631.76062OpenAlexW2069047297MaRDI QIDQ1094979

David S. Ross

Publication date: 1987

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-9991(87)90135-5

zbMATH Keywords

compressible flowsource distributionfree boundary supercritical wing design codemodelling an engine nacelle

Mathematics Subject Classification ID

Transonic flows (76H05) Basic methods in fluid mechanics (76M99)

Cites Work

• Supercritical wing sections II. A handbook
• Computation of wave drag for transonic flow
• Supercritical wing sections. III
• A theory of supercritical wing sections, with computer programs and examples
• Design of supercritical swept wings
• Numerical Calculation of Transonic Potential Flow about Wing-Body Combinations
• Calculation of plane steady transonic flows

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