NASA NTRS · 19800001880
Integration of ejectors into high-speed aircraft
Abstract
The integration of ejectors into forebodies is considered for transonic and supersonic flight. Topics discussed include mixing flow in ducts, prediction of flow fields and external aerodynamics.
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Duvvuri, T.. 1979-09-01. Integration of ejectors into high-speed aircraft. https://ntrs.nasa.gov/citations/19800001880
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