The flow over delta wings at low speeds with leading edge separation

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dc.contributor.authorMarsden, D. J.
dc.contributor.authorSimpson, R. W.
dc.contributor.authorRainbird, W. J.
dc.date.accessioned2009-12-18T11:46:54Z
dc.date.available2009-12-18T11:46:54Z
dc.date.issued1958-02
dc.description.abstractA low speed investigation of the flow over a 40 degree apex angle delta wing with sharp leading edges had been made in order to ascertain details of the flow in the viscous region near the leading edge of the suction surface of the wing. A physical picture of the flow was obtained from the surface flow and a smoke technique of flow visualization, combined with detailed measurements of total head, dynamic pressure, flow directions and vortex core positions in the flow above the wing.en_UK
dc.identifier.citationMarsden, D.J; Simpson, R.W; Rainbird W.J; The flow over delta wings at low speeds with leading edge separation, College of Aeronautics, 1958en_UK
dc.identifier.urihttp://hdl.handle.net/1826/4081
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCollege of Aeronautics Reporten_UK
dc.relation.ispartofseries114en_UK
dc.relation.ispartofseriesCOA/114en_UK
dc.titleThe flow over delta wings at low speeds with leading edge separationen_UK
dc.typeReporten_UK

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