Author Description

The analysis procedure of an existing computer program was extended to include rotor blade sweep, to model the flow more accurately at the rotor exit, and to provide more detail to the loss model. The modeling changes are described and all analysis equations and procedures are presented. Program input and output are described and are illustrated by an example problem. Results obtained from this program and from a previous program are compared with experimental data. Meitner, P. L. and Glassman, A. J. Glenn Research Center NASA-TP-2199, NAS 1.60:2199, AVRADCOM-TR-83-C-4 RTOP 535-05-12