Summary of NASA Aerodynamic and Heat Transfer Studies in Turbine Vanes and Blades National Aeronautics and Space Administration

Format:

Conference/Event

Author/Creator:

Moffitt, Thomas P., author.

Conference Name:

Aerospace Engineering and Manufacturing Meeting (1976-11-30 : San Diego, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1976

Summary:

Aerodynamic effects of trailing edge geometry, hole size, angle, spacing, and shape have been studied in two- and three-dimensional cascades and in a warm turbine test series. Heat transfer studies have been carried out in various two- and three-dimensional test facilities in order to provide corresponding heat transfer data. Results are shown in terms of cooling effectiveness and aerodynamic efficiency for various coolant fractions, coolant-primary temperature ratios, and cooling configurations

Notes:

Vendor supplied data

Publisher Number:

760917

Access Restriction:

Restricted for use by site license