| Sensing and Active Flow Control for Advanced Bwb Propulsion-Airframe Integration Concepts Contributor(s): Fleming, John (Author), Nasa Technical Reports Server (Ntrs) (Created by), Et Al (Created by) |
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ISBN: 1289250405 ISBN-13: 9781289250409 Publisher: Bibliogov OUR PRICE: $20.66 Product Type: Paperback Published: July 2013 |
| Additional Information |
| BISAC Categories: - Political Science |
| Physical Information: 0.32" H x 7.44" W x 9.69" (0.62 lbs) 150 pages |
| Descriptions, Reviews, Etc. |
| Publisher Description: 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. |