Title: Sensing and Active Flow Control for Advanced BWB Propulsion-Airframe Integration Concepts
Publisher: Bibliogov
Publication Date: 2013
Language: English
ISBN 10: 1289250405
ISBN 13: 9781289250409
Binding: Soft cover
Condition: New

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Synopsis

In order to realize the substantial performance benefits of serpentine boundary layer ingesting diffusers, this study investigated the use of enabling flow control methods to reduce engine-face flow distortion. Computational methods and novel flow control modeling techniques were utilized that allowed for rapid, accurate analysis of flow control geometries. Results were validated experimentally using the Techsburg Ejector-based wind tunnel facility; this facility is capable of simulating the high-altitude, high subsonic Mach number conditions representative of BWB cruise conditions.

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