Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Spitflow For Two Genetic High Performance Aircraft Models
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Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Spitflow For Two Genetic High Performance Aircraft Models
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Author : Eric F. Charlton
language : en
Publisher:
Release Date : 1998
Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Spitflow For Two Genetic High Performance Aircraft Models written by Eric F. Charlton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Spitflow For Two Generic High Performance Aircraft Models
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Author : Eric F. Charlton
language : en
Publisher:
Release Date : 1998
Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Spitflow For Two Generic High Performance Aircraft Models written by Eric F. Charlton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Computational fluid dynamics categories.
Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Splitflow For Two Generic High Performance Aircraft Models
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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher: Independently Published
Release Date : 2018-10-29
Numerical Stability And Control Analysis Towards Falling Leaf Prediction Capabilities Of Splitflow For Two Generic High Performance Aircraft Models written by National Aeronautics and Space Adm Nasa and has been published by Independently Published this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-10-29 with categories.
Aerodynamic analysis are performed using the Lockheed-Martin Tactical Aircraft Systems (LMTAS) Splitflow computational fluid dynamics code to investigate the computational prediction capabilities for vortex-dominated flow fields of two different tailless aircraft models at large angles of attack and sideslip. These computations are performed with the goal of providing useful stability and control data to designers of high performance aircraft. Appropriate metrics for accuracy, time, and ease of use are determined in consultations with both the LMTAS Advanced Design and Stability and Control groups. Results are obtained and compared to wind-tunnel data for all six components of forces and moments. Moment data is combined to form a "falling leaf" stability analysis. Finally, a handful of viscous simulations were also performed to further investigate nonlinearities and possible viscous effects in the differences between the accumulated inviscid computational and experimental data. Charlton, Eric F. Langley Research Center
An Evaluation Of Aerodynamic Prediction Methods Applied To The Xb 70 For Use In High Speed Aircraft Stability And Control System Design
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Author : Valery Razgonyaev
language : en
Publisher:
Release Date : 1995
An Evaluation Of Aerodynamic Prediction Methods Applied To The Xb 70 For Use In High Speed Aircraft Stability And Control System Design written by Valery Razgonyaev 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.
Second Quarterly Report On The Application Of Modified Stepwise Regression For The Estimation Of Aircraft Stability And Control Parameters
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Author : H. A. Hinds
language : en
Publisher:
Release Date : 1989
Second Quarterly Report On The Application Of Modified Stepwise Regression For The Estimation Of Aircraft Stability And Control Parameters written by H. A. Hinds and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Airplanes categories.