Open AccessArtificial viscosity method for the design of supercritical airfoils. [Analysis code H]
Author(s) -
G. B. McFadden
Publication year - 1979
Language(s) - English
Resource type - Reports
DOI - 10.2172/5850356
Subject(s) - airfoil , aerodynamics , transonic , aerospace engineering , wing , code (set theory) , supercritical fluid , wave drag , computer science , fuel efficiency , airplane , drag , design methods , field (mathematics) , mechanical engineering , engineering , physics , mathematics , set (abstract data type) , thermodynamics , programming language , pure mathematics
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