Design and Test of a Small, High-Pressure Ratio, Axial Compressor with Tandem and Swept Stators 720713
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.
Citation: Paine, C., "Design and Test of a Small, High-Pressure Ratio, Axial Compressor with Tandem and Swept Stators," SAE Technical Paper 720713, 1972, https://doi.org/10.4271/720713. Download Citation
Author(s):
Charles J. Paine
Pages: 13
Event:
National Farm, Construction, Industrial Machinery, Powerplant Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Compressors
Propellers and rotors
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