Dynamics of High-Bypass-Engine Thrust Reversal Using a Variable-Pitch Fan
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781724977014


Pages:   38
Publication Date:   09 August 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Dynamics of High-Bypass-Engine Thrust Reversal Using a Variable-Pitch Fan


Overview

The test program demonstrated that successful and rapid forward-to reverse-thrust transients can be performed without any significant engine operational limitations for fan blade pitch changes through either feather pitch or flat pitch. For through-feather-pitch operation with a flight inlet, fan stall problems were encountered, and a fan blade overshoot technique was used to establish reverse thrust. Schaefer, J. W. and Sagerser, D. R. and Stakolich, E. G. Glenn Research Center NASA-TM-X-3524, E-9026 RTOP 505-05...

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 28.00cm
Weight:   0.115kg
ISBN:  

9781724977014


ISBN 10:   1724977016
Pages:   38
Publication Date:   09 August 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   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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