Applied Mechanics Reviews PDF Download
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Author:
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ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
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Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 628
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Book Description
Author:
Publisher:
ISBN:
Category : Engineering
Languages : en
Pages : 504
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 660
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Neal Tetervin
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 192
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Book Description
The Magnus force is found by adding the boundary layer displacement surface to the body and then calculating the force on the resulting non- axisymmetric body. The displacement surface is calculated by the simultaneous integration of a differential equation for a streamline, two partial-differential boundary layer integral-momentum equations with the boundary layer thickness and the tangent of the angle between the local direction of the surface friction and potential flow streamline as dependent variables, and a partial differential equation for the displacement surface thickness. The method is applied to a half-ellipsoid of fineness ratio 5 at 4 degrees angle of attack. Slender-body theory is used to calculate the force.
Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 636
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 748
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Author: William C. Ragsdale
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ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 160
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Book Description
Pitot pressure surveys were made of the laminar boundary layer on an ogive-cylinder model at Mach 3.02 and 4.10. Surveys were made at five stations along the model, at angles of attack of zero and four degrees, with and without spin. Tests with spin were performed at Mach 3.02. The pitot pressure data has been used to compute boundary-layer velocity profiles, and results from two data-reduction procedures are presented. Some comparisons are made with theoretical velocity profiles for the zero spin, zero angle-of-attack case. (Author).
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 618
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Author: Valentine Korah
Publisher:
ISBN:
Category : Antitrust law
Languages : en
Pages : 2354
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Author:
Publisher: Academic Press
ISBN: 0080563821
Category : Technology & Engineering
Languages : en
Pages : 425
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Book Description
Advances in Applied Mechanics
