Summary of design and blade-element performance data for 12 axial-flow pump rotor configurations / by Max J. Miller [and four others].

Format:

Book

Government document

Author/Creator:

Miller, Max J., author.

Contributor:

United States. National Aeronautics and Space Administration, issuing body.

Series:

NASA technical note ; D-7074.

NASA/TN ; D-7074

Language:

English

Subjects (All):

Pumping machinery--Dynamics--Computer simulation.

Pumping machinery.

Blades--Design and construction.

Rotors--Design and construction.

Physical Description:

1 online resource (iii, 214 pages) : illustrations.

Place of Publication:

Washington, D.C. : National Aeronautics and Space Administration, January 1973.

Summary:

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.

Notes:

"January 1973."

Includes bibliographical references (pages 213-214).

Description based on online resource, PDF version; title from title page (NASA, viewed on June 1, 2021).

OCLC:

20650453