Nacelle Installation Effects on Propeller Blade Surface Pressure Distributions University of Southampton England

Format:

Conference/Event

Author/Creator:

Hurst, D. W., author.

Conference Name:

Aerospace Technology Conference & Exposition (1987-10-05 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1987

Summary:

A system capable of measuring the time averaged surface pressure distributions on rotating model propeller blades has been developed. A wide range of test conditions have been investigated and results displaying the effects of changes in blade setting angle, advance ratio and number of blades on the blade surface pressures are presented. In addition, the system has been used to experimentally investigate the influence of nacelle type afterbodies on the propeller blade pressure distribution

Notes:

Vendor supplied data

Publisher Number:

871773

Access Restriction:

Restricted for use by site license