NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Prediction of turbulent shear layers in turbomachinesThe characteristics of turbulent shear layers in turbomachines are compared with the turbulent boundary layers on airfoils. Seven different aspects are examined. The limits of boundary layer theory are investigated. Boundary layer prediction methods are applied to analysis of the flow in turbomachines.
Document ID
19750003112
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bradshaw, P. (Imperial Coll. of Science and Technology London, United Kingdom)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Publication Information
Publication: Pennsylvania State Univ. Fluid Mech., Acoustic, and Design of Turbomachinery, Pt. 1
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
75N11184
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19750003102Collected WorksFluid mechanics, acoustics, and design of turbomachinery, part 119750003102Collected WorksFluid mechanics, acoustics, and design of turbomachinery, part 1
No Preview Available