NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Blade DesignThe design of turbine blading is considered that will produce the flow angles and velocities required by velocity diagrams consistent with the desired efficiency and/or number of stages. The determination of the size, shape, and spacing of the blades is fundamental.
Document ID
19740025364
Acquisition Source
Glenn Research Center
Document Type
Other - Technical Report
Authors
Warner L. Stewart (Glenn Research Center Cleveland, United States)
Arthur J. Glassman (Glenn Research Center Cleveland, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Turbine Design and Application: Volume 2
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Propulsion And Power
Accession Number
74N33477
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19740025363Collected WorksTurbine Design and Application: Volume 2
No Preview Available