Recent Developments in Ejector Design for V/STOL Aircraft The de Havilland Aircraft of Canada, Limited

Format:

Conference/Event

Author/Creator:

Whittley, D. C., author.

Conference Name:

Aerospace Congress & Exposition (1984-10-15 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1984

Summary:

Two categories of ejector design have been investigated at de Havilland Aircraft of Canada:The paper reviews the underlying physical principles of the ejector type of thrust augmentor and suggests a logical procedure for development and optimization by experimental means. Methods of data analysis are shown which provide the foundation for empirical design and some examples of performance are given for each of the two ejector categories defined above. In addition, a new form of primary nozzle is described which serves to distribute the jet and promote fast mixing in the ejector throat

Notes:

Vendor supplied data

Publisher Number:

841498

Access Restriction:

Restricted for use by site license