Title: Some wind-tunnel results of an investigation of the flutter of sweptback- and triangular-wing models at Mach number 1.3
Abstract: Memorandum presenting flutter tests of untapered, low-aspect-ratio, sweptback-wing models and of triangular-wing models of solid magnesium, aluminum, and steel construction in an intermittent supersonic wind tunnel at Mach number 1.3. Flutter data are presented for 31 sweptback wing models and 24 triangular-wing models. The flutter boundaries are indicated on plots of streamwise thickness ratio and aspect ratio.
Publication Year: 1952
Publication Date: 1952-05-22
Language: en
Type: article
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Cited By Count: 3
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