Publication Date:
2019-06-28
Description:
This report summarizes some NASA Lewis (i.e., government owned) computer codes capable of being used for airbreathing propulsion system studies to determine the design geometry and to predict the design/off-design performance of compressors and turbines. These are not CFD codes; velocity-diagram energy and continuity computations are performed fore and aft of the blade rows using meanline, spanline, or streamline analyses. Losses are provided by empirical methods. Both axial-flow and radial-flow configurations are included.
Keywords:
AERODYNAMICS
Type:
NASA-CR-198433
,
NAS 1.26:198433
,
E-10041
,
NIPS-95-06493
Format:
application/pdf