Blade-element Performance of 0.7 Hub-tip Radius Ratio Axial-flow-pump Rotor with Tip Diffusion Factor of 0.43

Blade-element Performance of 0.7 Hub-tip Radius Ratio Axial-flow-pump Rotor with Tip Diffusion Factor of 0.43 PDF Author: James E. Crouse
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 48

Get Book Here

Book Description

Blade-element Performance of 0.7 Hub-tip Radius Ratio Axial-flow-pump Rotor with Tip Diffusion Factor of 0.43

Blade-element Performance of 0.7 Hub-tip Radius Ratio Axial-flow-pump Rotor with Tip Diffusion Factor of 0.43 PDF Author: James E. Crouse
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 48

Get Book Here

Book Description


Blade Element Performance of Axial-flow Pump Rotor with Blade Tip Diffusion Factor of 0.66

Blade Element Performance of Axial-flow Pump Rotor with Blade Tip Diffusion Factor of 0.66 PDF Author: Max J. Miller
Publisher:
ISBN:
Category : Axial flow pumps
Languages : en
Pages : 44

Get Book Here

Book Description


Design and Overall Performance of an Axial-flow-pump Rotor with a Blade Tip Diffusion Factor of 0.43

Design and Overall Performance of an Axial-flow-pump Rotor with a Blade Tip Diffusion Factor of 0.43 PDF Author: James E. Crouse
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 40

Get Book Here

Book Description


Design and Performance of an 0.8-hub-tip-ratio Axial-flow Pump Rotor with a Blade-tip Diffusion Factor of 0.55

Design and Performance of an 0.8-hub-tip-ratio Axial-flow Pump Rotor with a Blade-tip Diffusion Factor of 0.55 PDF Author: Donald C. Urasak
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Get Book Here

Book Description


Design and Performance of a 0.9 Hub-tip-ratio Axial Flow Pump Rotor with a Blade-tip Diffusion Factor of 0.63

Design and Performance of a 0.9 Hub-tip-ratio Axial Flow Pump Rotor with a Blade-tip Diffusion Factor of 0.63 PDF Author: Donald C. Urasek
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

Get Book Here

Book Description


Blade Element Performance of Axial-flow Pump Rotor with Blade Tip Diffusion Factor of 0.66

Blade Element Performance of Axial-flow Pump Rotor with Blade Tip Diffusion Factor of 0.66 PDF Author: Max J. Miller
Publisher:
ISBN:
Category : Axial flow pumps
Languages : en
Pages : 33

Get Book Here

Book Description


Design and Overall Performance of an Axial-flow Pump Rotor with a Blade-tip Diffusion Factor of 0.66

Design and Overall Performance of an Axial-flow Pump Rotor with a Blade-tip Diffusion Factor of 0.66 PDF Author: Max J. Miller
Publisher:
ISBN:
Category : Blades
Languages : en
Pages : 36

Get Book Here

Book Description


NASA Technical Note

NASA Technical Note PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 394

Get Book Here

Book Description


Experimental Investigation of a 0.35 Hub-Tip Radius Ratio Transonic Axial Flow Rotor Designed for 40 Pounds Per Second Per Square Foot with a Design Tip Diffusion Factor of 0.20

Experimental Investigation of a 0.35 Hub-Tip Radius Ratio Transonic Axial Flow Rotor Designed for 40 Pounds Per Second Per Square Foot with a Design Tip Diffusion Factor of 0.20 PDF Author: Paul T. Yasaki
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44

Get Book Here

Book Description


Summary of Design and Blade-element Performance Data for 12 Axial-flow Pump Rotor Configurations

Summary of Design and Blade-element Performance Data for 12 Axial-flow Pump Rotor Configurations PDF Author: Max J. Miller
Publisher:
ISBN:
Category : Blades
Languages : en
Pages : 228

Get Book Here

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.