Fluid Mechanics, Drag Reduction and Advanced Configuration Aeronautics

Author:   National Aeronautics and Space Adm Nasa
Publisher:   Independently Published
ISBN:  

9781724111579


Pages:   36
Publication Date:   27 September 2018
Format:   Paperback
Availability:   In stock   Availability explained
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Fluid Mechanics, Drag Reduction and Advanced Configuration Aeronautics


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Overview

This paper discusses Advanced Aircraft configurational approaches across the speed range, which are either enabled, or greatly enhanced, by clever Flow Control. Configurations considered include Channel Wings with circulation control for VTOL (but non-hovering) operation with high cruise speed, strut-braced CTOL transports with wingtip engines and extensive ('natural') laminar flow control, a midwing double fuselage CTOL approach utilizing several synergistic methods for drag-due-to-lift reduction, a supersonic strut-braced configuration with order of twice the L/D of current approaches and a very advanced, highly engine flow-path-integrated hypersonic cruise machine. This paper indicates both the promise of synergistic flow control approaches as enablers for 'Revolutions' in aircraft performance and fluid mechanic 'areas of ignorance' which impede their realization and provide 'target-rich' opportunities for Fluids Research. Bushnell, Dennis M. Langley Research Center NASA/TM-2000-210646, NAS 1.15:210646, L-18055

Full Product Details

Author:   National Aeronautics and Space Adm Nasa
Publisher:   Independently Published
Imprint:   Independently Published
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 27.90cm
Weight:   0.109kg
ISBN:  

9781724111579


ISBN 10:   1724111574
Pages:   36
Publication Date:   27 September 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   In stock   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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