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A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up

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A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up

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Author : Mark S. Chaffin
language : en
Publisher:
Release Date : 1995

A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up written by Mark S. Chaffin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with categories.

A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up

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Author : Mark Steven Chaffin
language : en
Publisher:
Release Date : 1995

A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up written by Mark Steven Chaffin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Navier-Stokes equations categories.

Nasa Technical Memorandum

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Author :
language : en
Publisher:
Release Date : 1996

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Aeronautics categories.

A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up

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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-28

A Guide To The Use Of The Pressure Disk Rotor Model As Implemented In Ins3d Up written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-06-28 with categories.

This is a guide for the use of the pressure disk rotor model that has been placed in the incompressible Navier-Stokes code INS3D-UP. The pressure disk rotor model approximates a helicopter rotor or propeller in a time averaged manner and is intended to simulate the effect of a rotor in forward flight on the fuselage or the effect of a propeller on other aerodynamic components. The model uses a modified actuator disk that allows the pressure jump across the disk to vary with radius and azimuth. The cyclic and collective blade pitch angles needed to achieve a specified thrust coefficient and zero moment about the hub are predicted. The method has been validated with experimentally measured mean induced inflow velocities as well as surface pressures on a generic fuselage. Overset grids, sometimes referred to as Chimera grids, are used to simplify the grid generation process. The pressure disk model is applied to a cylindrical grid which is embedded in the grid or grids used for the rest of the configuration. This document will outline the development of the method, and present input and results for a sample case. Chaffin, Mark S. Unspecified Center NAS1-19672; RTOP 505-59-36-01...

Nasa Langley Scientific And Technical Information Output 1995

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Author :
language : en
Publisher:
Release Date : 1996

Nasa Langley Scientific And Technical Information Output 1995 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Astronautics categories.

This document is a compilation of the scientific and technical information that the Langley Research Center has produced during the calendar year 1995. Included are citations for formal reports, high-numbered conference publications, high-numbered technical memorandums, contractor reports, journal articles and other publications, meeting presentations, technical talks, computer programs, tech briefs, and patents.