Description of ADPAC

Description of ADPAC PDF Author: Mikael Sternad
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Description of ADPAC

Description of ADPAC PDF Author: Mikael Sternad
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Book Description


ADPAC V1.0: User's Manual

ADPAC V1.0: User's Manual PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 270

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Task 7: ADPAC User's Manual

Task 7: ADPAC User's Manual PDF Author: E. J. Hall
Publisher:
ISBN:
Category :
Languages : en
Pages : 272

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The overall objective of this study was to develop a 3-D numerical analysis for compressor casing treatment flowfields. The current version of the computer code resulting from this study is referred to as ADPAC (Advanced Ducted Propfan Analysis Codes-Version 7). This report is intended to serve as a computer program user's manual for the ADPAC code developed under Tasks 6 and 7 of the NASA Contract. The ADPAC program is based on a flexible multiple- block grid discretization scheme permitting coupled 2-D/3-D mesh block solutions with application to a wide variety of geometries. Aerodynamic calculations are based on a four-stage Runge-Kutta time-marching finite volume solution technique with added numerical dissipation. Steady flow predictions are accelerated by a multigrid procedure. An iterative implicit algorithm is available for rapid time-dependent flow calculations, and an advanced two equation turbulence model is incorporated to predict complex turbulent flows. The consolidated code generated during this study is capable of executing in either a serial or parallel computing mode from a single source code. Numerous examples are given in the form of test cases to demonstrate the utility of this approach for predicting the aerodynamics of modem turbomachinery configurations.

Preliminary Findings in Certification of ADPAC

Preliminary Findings in Certification of ADPAC PDF Author: Thomas J. Barber
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 5: Unsteady Counterrotation Ducted Propfan Analysis. Computer Program User's Manual

Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 5: Unsteady Counterrotation Ducted Propfan Analysis. Computer Program User's Manual PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 220

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Recent Advances in Computer-aided Control Systems Engineering

Recent Advances in Computer-aided Control Systems Engineering PDF Author: Mohammad Jamshidi
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 482

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TADS: A CFD-Based Turbomachinery Analysis and Design System with GUI: Methods and Results

TADS: A CFD-Based Turbomachinery Analysis and Design System with GUI: Methods and Results PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 164

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TADS--A CFD-Based Turbomachinery Analysis and Design System with GUI: User's Manual

TADS--A CFD-Based Turbomachinery Analysis and Design System with GUI: User's Manual PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

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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

Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems. Task 8: Cooling Flow/heat Transfer Analysis User's Manual PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 368

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TADS: A CFD-based Turbomachinery and Analysis Design System with GUI. Volume 1: Method and Results

TADS: A CFD-based Turbomachinery and Analysis Design System with GUI. Volume 1: Method and Results PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 126

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