Design and Test of a Small, High-Pressure Ratio, Axial Compressor with Tandem and Swept Stators

Format:

Conference/Event

Author/Creator:

Paine, Charles J., author.

Conference Name:

National Farm, Construction, Industrial Machinery, Powerplant Meeting (1972-09-11 : Milwaukee, Wisconsin, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1972

Summary:

A small (22.2 lb/s), high-pressure ratio (1.83), axial compressor stage with a tandem stator has been designed and tested. The rotor was based on a 0.359-scale of a design made for NASA. The tandem stator consisted of a backward-swept first stage and a rectilinear (zero sweep) second stage. The scaled-stage overall performance was comparable to that of the full-size stage

Notes:

Vendor supplied data

Publisher Number:

720713

Access Restriction:

Restricted for use by site license