Accession Number:

ADP007683

Title:

Application of S1BYL2 to the AGARD WG18 Compressor Test Cases,

Descriptive Note:

Corporate Author:

ROYAL AEROSPACE ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)

Personal Author(s):

• Calvert, W. J.

Report Date:

1992-02-01

Pagination or Media Count:

16.0

Abstract:

S1BYL2 is an inviscid-viscous blade-to-blade method for calculating the detailed aerodynamics and overall performance of compressor blades. It may be applied either on its own to predict the flow for individual blade sections, such as the mid span of a linear cascade, or in conjunction with a throughflow calculation to predict the performance of a complete axial compressor.

Descriptors:

• *COMPRESSOR BLADES
• *COMPUTER PROGRAMS
• AERODYNAMICS
• BLADES
• COMPRESSORS
• FLOW
• COMPUTATIONS

Subject Categories:

• Fluid Mechanics
• Computer Programming and Software
• Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE