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Unsteady Features of Jets in Lift and Cruise Modes for VTOL Aircraft McDonnell Douglas Research Laboratories

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kibens, V., author.
Conference Name:
SAE International Powered Lift Conference and Exposition (1987-12-07 : Santa Clara, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1987
Summary:
Experiments were performed to simulate jet plume effects associated with VTOL aircraft in takeoff and cruise modes. A water facility was used to investigate the influence of inclination angle and separation distance on the three-dimensional fountain flowfield generated by two impinging jets operating at a jet Reynolds number of 250,000. Substantial differences in the flow features were observed for different spacings between the jets. Plume effects in cruise mode were simulated by a supersonic unheated jet parallel to a wall. Variation of the distance between the wall and the edge of the plume is shown to have a major controlling effect on the supersonic screech instability
Notes:
Vendor supplied data
Publisher Number:
872359
Access Restriction:
Restricted for use by site license

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