Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 8 PDF Download
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724265586
Category :
Languages : en
Pages : 366
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Book Description
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...
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724265586
Category :
Languages : en
Pages : 366
Get Book Here
Book Description
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...
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724265432
Category :
Languages : en
Pages : 202
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Book Description
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. The primary validation case was the film cooled C3X vane. The cooling hole modeling included both a porous region and grid in each discrete hold. Predictions for these models as well as smooth wall compared well with the experimental data. Hall, Edward J. and Topp, David A. and Heidegger, Nathan J. and Delaney, Robert A. Unspecified Center NASA-CR-195359, E-9024, NAS 1.26:195359 NAS3-25270; RTOP 538-03-11...
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Category :
Languages : en
Pages : 368
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Category :
Languages : en
Pages : 206
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Author: Edward J. Hall
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Category : Aerodynamics
Languages : en
Pages : 354
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Category : Aeronautics
Languages : en
Pages : 548
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Category :
Languages : en
Pages : 88
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Category : Government publications
Languages : en
Pages : 1450
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Category :
Languages : en
Pages : 80
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Category : Government publications
Languages : en
Pages : 1638
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