Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 8: Cooling Flow/Heat Transfer Analysis User's Manual
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781724265586


Pages:   368
Publication Date:   25 July 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 8: Cooling Flow/Heat Transfer Analysis User's Manual


Overview

The focus of this task was to validate the ADPAC code for heat transfer calculations. To accomplish this goal, the ADPAC code was modified to allow for a Cartesian coordinate system capability and to add boundary conditions to handle spanwise periodicity and transpiration boundaries. This user's manual describes how to use the ADPAC code as developed in Task 5, NAS3-25270, including the modifications made to date in Tasks 7 and 8, NAS3-25270. Hall, Edward J. and Topp, David A. and Heidegger, Nathan J. and Delaney, Robert A. Unspecified Center NASA-CR-195360, E-9025, NAS 1.26:195360 NAS3-25270; RTOP 538-03-11...

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 1.90cm , Length: 27.90cm
Weight:   0.853kg
ISBN:  

9781724265586


ISBN 10:   172426558
Pages:   368
Publication Date:   25 July 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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