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Sensing and Active Flow Control for Advanced BWB Propulsion-Airframe Integration Concepts

Sensing and Active Flow Control for Advanced BWB Propulsion-Airframe Integration Concepts

Paperback

General Political Science

ISBN10: 1289250405
ISBN13: 9781289250409
Publisher: Bibliogov
Published: Jul 29 2013
Pages: 150
Weight: 0.62
Height: 0.32 Width: 7.44 Depth: 9.69
Language: English
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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General Political Science