Numerical Computations Of Supersonic Flow Over A Square Cross Section Missile
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Numerical Computations Of Supersonic Flow Over A Square Cross Section Missile
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Author :
language : en
Publisher:
Release Date : 2005
Numerical Computations Of Supersonic Flow Over A Square Cross Section Missile written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Air flow categories.
This report describes a computational study undertaken to determine the aerodynamics of a nonaxisymmetric missile with a square cross section. Numerical solutions have been obtained at supersonic speeds for various roll orientations and angles of attack using a two-equation Reynolds-averaged Navier-Stokes turbulence model. Numerical results show the qualitative features (vortices and cross-flow separation regions) of the flow field at various stream wise positions along the missile configurations. Aerodynamic coefficients have been obtained from the computed solutions and found to match well with the available experimental data for these configurations. These numerical results show the ability of computational fluid dynamics techniques to accurately predict the aerodynamics of nonaxisymmetric missiles with a square cross section.
Numerical Computations Of Supersonic Flow Over A Square Cross Section Missile
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Author :
language : en
Publisher:
Release Date : 2005
Numerical Computations Of Supersonic Flow Over A Square Cross Section Missile written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with categories.
This report describes a computational study undertaken to determine the aerodynamics of a nonaxisymmetric missile with a square cross section. Numerical solutions have been obtained at supersonic speeds for various roll orientations and angles of attack using a two-equation Reynolds-averaged Navier-Stokes turbulence model. Numerical results show the qualitative features (vortices and cross-flow separation regions) of the flow field at various stream wise positions along the missile configurations. Aerodynamic coefficients have been obtained from the computed solutions and found to match well with the available experimental data for these configurations. These numerical results show the ability of computational fluid dynamics techniques to accurately predict the aerodynamics of nonaxisymmetric missiles with a square cross section.
Application Of Computational Fluid Dynamics To A Monoplane Fixed Wing Missile With Elliptic Cross Sections
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Author : Karen R. Heavey
language : en
Publisher:
Release Date : 2005
Application Of Computational Fluid Dynamics To A Monoplane Fixed Wing Missile With Elliptic Cross Sections written by Karen R. Heavey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Computational fluid dynamics categories.
This report describes a computational study undertaken to investigate the performance of the CFD++ flow solver for prediction of nonlinear aerodynamics of a complex finned missile using structured hexahedral and unstructured tetrahedral grids. A monoplane fixed-wing missile with elliptic cross sections provided a geometrically complex model. Numerical solutions were obtained for this configuration at supersonic speed for various roll orientations, angles of attack, and jaw angles. Steady-state solutions were obtained using a three-dimensional Reynolds-Averaged Navier-Stokes solver with a two-equation turbulence model. Numerical results show the qualitative features of the flow fields at various cross-sectional and streamwise positions along the computational model of the missile. Aerodynamic coefficients were extracted from the computed solutions and found to match well with the available experimental data for these configurations. These numerical results show the effectiveness of using computational fluid dynamics techniques to produce an accurate prediction of the aerodynamics of geometrically complete configurations.
Proceedings Of The International Conference On Systems Science Control Communication Engineering And Technology 2015
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Author : Kokula Krishna Hari K
language : en
Publisher: Association of Scientists, Developers and Faculties (ASDF)
Release Date : 2015-08-10
Proceedings Of The International Conference On Systems Science Control Communication Engineering And Technology 2015 written by Kokula Krishna Hari K and has been published by Association of Scientists, Developers and Faculties (ASDF) this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-08-10 with Computers categories.
ICSSCCET 2015 will be the most comprehensive conference focused on the various aspects of advances in Systems, Science, Management, Medical Sciences, Communication, Engineering, Technology, Interdisciplinary Research Theory and Technology. This Conference provides a chance for academic and industry professionals to discuss recent progress in the area of Interdisciplinary Research Theory and Technology. Furthermore, we expect that the conference and its publications will be a trigger for further related research and technology improvements in this important subject. The goal of this conference is to bring together the researchers from academia and industry as well as practitioners to share ideas, problems and solutions relating to the multifaceted aspects of Interdisciplinary Research Theory and Technology.
High Angle Of Attack Aerodynamics
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Author : Josef Rom
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06
High Angle Of Attack Aerodynamics written by Josef Rom and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-06 with Science categories.
The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1948
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Mechanics, Applied categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1999
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Aeronautics categories.
An Improved Semiempirical Method For Calculating Aerodynamics Of Missiles With Noncircular Bodies
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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1997
An Improved Semiempirical Method For Calculating Aerodynamics Of Missiles With Noncircular Bodies written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Aerodynamics categories.
Monthly Catalog Of United States Government Publications
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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1959
Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Government publications categories.
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.