NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A rapid blade-to-blade solution for use in turbomachinery designA rapid technique for solving the blade-to-blade turbomachinery flow problem was developed. Approximate governing flow equations, which include the effects of compressibility, radius change, rotation, and variable stream sheet thickness are solved using a panel method. The development and solution of these equations are described. Sample calculations are presented to illustrate the method's capabilities and accuracy.
Document ID
19830004807
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcfarland, E. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
E-1445
NAS 1.15:83010
NASA-TM-83010
Report Number: E-1445
Report Number: NAS 1.15:83010
Report Number: NASA-TM-83010
Meeting Information
Meeting: Ann. Intern. Gas Turbine Conf.
Location: Phoenix, AZ
Country: United States
Start Date: March 27, 1983
End Date: March 31, 1983
Sponsors: ASME
Accession Number
83N13077
Funding Number(s)
PROJECT: RTOP 505-32-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available