Simple technique presented for correcting singularities predicted by this theory at subsonic edges; thus, M.J.LIGHTHILL's rule for speeds on round nosed airfoils in incompressible flow is extended to higher approximations, compressible flow, 3-dimensional wings, sharp edges, and slender bodies of revolution.
Subsonic edges in thin-wing and slender-body theory
NACA -- Tech Note
1954
26 pages
Report
Englisch
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