An engineering approach to the inverse transonic wing design problem

DOI10.1002/CNM.1630020108zbMath0591.76104OpenAlexW2021587015MaRDI QIDQ3720150

Jeffrey Mantel, E. Greff

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.1630020108

zbMATH Keywords

high accuracycurvature influencedirect-inverse design of supercritical wing sectionsDIVA methodflows with strong shocksIncremental improvements of wing performanceinitial wing shapetransonic codetwo-dimensional methodwake thickness

Mathematics Subject Classification ID

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

Related Items (2)

An inverse method with regularity condition for transonic airfoil design ⋮ Computational methods for aerodynamic shape design

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