FIELD: experimental aerodynamics. SUBSTANCE: method is based on the configuration change of the diffuser neck. A vortex cord is created additionally and directed to the input cross-section of the diffuser. The latter has movable panels 1 forming input cross-section 2, input section 3, neck 4 and output section 5. EFFECT: improved operational characteristics. 2 cl, 2 dwg
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Authors
Dates
1995-02-09—Published
1990-01-22—Filed