Sensing And Active Flow Control For Advanced Bwb Propulsion-airframe Integration Concepts

by Nasa Technical Reports Server (ntrs)

2021-06-03 21:35:33

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 co... Read more
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. Less

Book Details

ISBN9781289250409

Compare Prices

Store Availability Book Format Condition Price
Indigo Books & Music In Stock Buy CAD 25.99
Indigo Books & MusicIn Stock
Format
Condition
Buy CAD 25.99
Available Discount
No Discount available

Join us and get access to all
your favourite books

Sign up for free and start exploring thousands of eBooks today.

Sign up for free