NASA Technical Note PDF Download
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Author:
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Category : Aeronautics
Languages : en
Pages : 814
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 814
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Book Description
Author: Richard F. Soltis
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Category : Centrifugal pumps
Languages : en
Pages : 44
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Book Description
Blade element performance of tandem bladed inducer tested in water.
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Category : Jet pumps
Languages : en
Pages : 132
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Book Description
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1330
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Book Description
Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1576
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Book Description
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1032
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ISBN:
Category : Government publications
Languages : en
Pages :
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Author: BHRA (Association)
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Category :
Languages : en
Pages : 148
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Book Description
Author:
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Category : Mechanics, Applied
Languages : en
Pages : 712
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Book Description
Author: Max J. Miller
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Category : Blades
Languages : en
Pages : 228
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Book Description
A collection of noncavitating blade-element performance data for 12 axial-flow pump rotor configurations is presented in tabular form. Rotor design philosophy, test apparatus and procedure, and data reduction and evaluation are discussed. A data storage and recall computer program is described. All but one of the rotor configurations considered were composed of double-circular-arc blade sections and were designed for high inlet relative flow angles. Hub-tip radius ranged from 0.40 to 0.90.
