Discharge Coefficients for Thick Plate Orifices with Approach Flow Perpendicular and Inclined to the Orifice Axis PDF Download
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Author: John E. Rohde
Publisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 36
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Book Description
Discharge nozzle coefficients for thick plate orifices with approach flow perpendicular and inclined to orifice axis.
Author: John E. Rohde
Publisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 36
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Book Description
Discharge nozzle coefficients for thick plate orifices with approach flow perpendicular and inclined to orifice axis.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 520
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 976
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 962
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 956
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 284
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Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 60
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Book Description
Water flow tests with circumferential inlet and outlet manifolds were conducted to determine factors affecting fluid distribution and pressure losses. Various orifice sizes and manifold geometries were tested over a range of flow velocities. With inlet manifolds, flow distribution was related directly to orifice discharge coefficients. A correlation indicated that nonuniform distribution resulted when the velocity head ratio at the orifice was not in the range of constant discharge coefficient. With outlet manifolds, nonuniform flow was related to static pressure variations along the manifold. Outlet manifolds had appreciably greater pressure losses than comparable inlet manifolds.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 368
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Book Description
