Accession Number:

ADP003073

Title:

Application of an Inviscid-Viscous Interaction Method to Transonic Compressor Cascades,

Descriptive Note:

Corporate Author:

NATIONAL GAS TURBINE ESTABLISHMENT FARNBOROUGH (ENGLAND)

Personal Author(s):

Report Date:

1983-09-01

Pagination or Media Count:

13.0

Abstract:

A recent ASME paper by the author described an inviscid-viscous interaction method to predict the blade-to-blade flow in axial compressors. This paper presents comparisons between the predictions from the method and experimental data from a number of transonic linear cascades. The cascades cover a wide range of duties, with inlet Mach numbers varying from 0.8 to 1.46 and flow deflections from 7 deg to 50 deg. Generally the predictions are in good agreement with the test data. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE