Compressible flow airfoil design using natural coordinates

DOI10.1016/0045-7825(93)90024-RzbMath0845.76083OpenAlexW2089712213MaRDI QIDQ1912179

Yanyan Li

Publication date: 22 September 1996

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(93)90024-r

zbMATH Keywords

potentialinverse problemstreamfunctiondifferential geometrytrailing edgeFrenet equationsbody-fitted coordinate transformationtwo-parameter iterative scheme

Mathematics Subject Classification ID

Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (1)

On the 3-D inverse potential target pressure problem. Part 1. Theoretical aspects and method formulation

Cites Work

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• Rotational compressible inverse design method for two-dimensional, internal flow configurations
• A three-dimensional modified strongly implicit procedure for heat conduction
• On the 3-D inverse potential target pressure problem. Part 1. Theoretical aspects and method formulation

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