Publication Date:
2019-06-28
Description:
Modifications made to the axial-flow compressor conceptual design code CSPAN are documented in this report. Endwall blockage and stall margin predictions were added. The loss-coefficient model was upgraded. Default correlations for rotor and stator solidity and aspect-ratio inputs and for stator-exit tangential velocity inputs were included in the code along with defaults for aerodynamic design limits. A complete description of input and output along with sample cases are included.
Keywords:
AERODYNAMICS
Type:
NASA-TM-106833
,
E-9394
,
NAS 1.15:106833
Format:
application/pdf