Contribution à l'étude expérimentale des lois de similitude en aérodynamique PDF Download
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Author: Albert Toussaint
Publisher:
ISBN:
Category :
Languages : fr
Pages : 0
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Author: Albert Toussaint
Publisher:
ISBN:
Category :
Languages : fr
Pages : 0
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Author: Albert Toussaint
Publisher:
ISBN:
Category :
Languages : fr
Pages : 103
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Author: Albert Toussaint
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ISBN:
Category :
Languages : fr
Pages : 0
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 714
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Chiefly translations from foreign aeronautical journals.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498
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Chiefly translations from foreign aeronautical journals.
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ISBN:
Category : Aeronautics
Languages : en
Pages : 764
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Chiefly translations from foreign aeronautical journals.
Author: H. Schlichting
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 604
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Book Description
Based on the universal laws of turbulent velocity distribution at rough and smooth walls, there is in the present work presented a method that allows surface roughness tests and in particular, measurements on the roughness of ship surfaces to be carried out in a much simpler manner. The types of roughness investigated were in the form of flat, rough plates installed in a square-section rectangular channel, the other three walls always being smooth. Twenty-one plates of various roughness were investigated, the roughness elements being the following: spheres of diameter 0.41 and 0.21, respectively, spherical segments, cones, and "short" and "long" angles.
Author: Albert Toussaint
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ISBN:
Category :
Languages : fr
Pages : 101
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Author: Karl Schüssler
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ISBN:
Category : Duralumin
Languages : en
Pages : 662
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This report presents the results of an investigation to determine the behavior of dural strip with flanged holes in the center when subjected to shear stresses. They buckle under a certain load just as a flat sheet. There is one optimum hole spacing and a corresponding buckling load in shear for each sheet width, sheet thickness, and flange form. Comparison with non-flanged sheets revealed a marked increase of buckling load in shear due to the flanging and a slightly greater displacement. Strips were clamped between two stationary end rails and one sliding center rail at which the shear is applied. The force was measured with a tension stirrup up to 20 tons and a compression dynamometer up to 10 tons. The displacement was recorded with the Zeiss dial gauge. The following were investigated: 1) effect of strip width; 2) strip thickness; 3) diameter of flanging; 4) depth of flanging; 5) and hole distance.
Author: David W. Taylor Model Basin
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ISBN:
Category : Shipbuilding
Languages : en
Pages : 60
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