Detailed Computational Procedure for Design of Cascade Blades with Prescribed Velocity Distributions in Compressible Potential Flows PDF Download
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Author: George R. Costello
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 56
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Book Description
The computational procedure includes several ways of adjusting the prescribed velocity to satisfy the restriction imposed by the method. Tables of coefficients are given for evaluating the necessary integrals, including the determination of the harmonic conjugate. Numerical examples are included.
Author: George R. Costello
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 56
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Book Description
The computational procedure includes several ways of adjusting the prescribed velocity to satisfy the restriction imposed by the method. Tables of coefficients are given for evaluating the necessary integrals, including the determination of the harmonic conjugate. Numerical examples are included.
Author: George R. Costello
Publisher:
ISBN:
Category :
Languages : en
Pages : 49
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Book Description
Author: George R. Costello
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 30
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Book Description
If the prescribed velocity distribution is not theoretically attainable, the method gives a way of modifying the distribution so as to obtain a blade shape.
Author: Arthur G. Hansen
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 51
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Book Description
A numerical procedure based on conformal-mappng theory is presented for design of an airfoil cascade with prescribed velocity distribution in incompressible flow. A set of tables is included as a guide for computations, and a numerical example is presented to illustrate specific solutions to problems arising in design of a cascade by this method.
Author: George R. Costello
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 11
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Book Description
If the prescribed velocity distribution is not theoretically attainable, the method gives a way of modifying the distribution so as to obtain a blade shape.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 24
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Book Description
Author: W. G. Lidman
Publisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages : 724
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Book Description
The sintering of chromium carbide under pressure was investigated in order to study the kinetics of grain growth and densification during this process. Densification was accompanied by grain growth, and density and grain size seem to be interdependent during this stage. Grain growth continued after densification was complete, and for this stage an activation energy for grain growth was obtained.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
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