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Analysis Of Free Flight Aerodynamic Range Data Of The 155mm M549 Projectile

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Analysis Of Free Flight Aerodynamic Range Data Of The 155mm M549 Projectile

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Author : United States. Army Armament Research and Development Command
language : en
Publisher:
Release Date : 1980

Analysis Of Free Flight Aerodynamic Range Data Of The 155mm M549 Projectile written by United States. Army Armament Research and Development Command and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with categories.

A Determination Of The Aerodynamic Coefficients Of The 155mm M549 Projectile

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Author : R. Kline
language : en
Publisher:
Release Date : 1974

A Determination Of The Aerodynamic Coefficients Of The 155mm M549 Projectile written by R. Kline and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Howitzers categories.

Technical Abstract Bulletin

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Author :
language : en
Publisher:
Release Date :

Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.

Sandrag

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Author : Walter P. Wolfe
language : en
Publisher:
Release Date : 1985

Sandrag written by Walter P. Wolfe and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with Angle of attack (Aerodynamics). categories.

A design method is presented for calculating the flow field and drag of bodies of revolution at zero angle of attack in incompressible flow. The body pressure distribution, viscous shear stress, and boundary layer separation point are calculated by a combination of potential flow method and boundary layer techniques. The portential solution is obtained by modeling the body with an axial distribution of source/sink elements who strengths very linearly along their length. Both the laminar and turbulent boundary layer solutions use momentum integral techniques which have been modified to account for the effects of surface roughness. An existing technique for estimating the location of transition was also modified to include surface roughness. Empirical correlations are developed to estimate the base pressure coefficient on a wide variety of geometries. Body surface pressure distributions and drag predictions are compared with experimental data for artillery projectiles, conical, and flared bodies. Very good agreement between the present method and experiment is obtained.

Tactical Missile Aerodynamics

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Author : M. R. Mendenhall
language : en
Publisher:
Release Date : 1992

Tactical Missile Aerodynamics written by M. R. Mendenhall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Guided missiles categories.

11th International Symposium On Ballistics Propulsion Dynamics Launch Dynamics Flight Dynamics

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Author :
language : en
Publisher:
Release Date : 1989

11th International Symposium On Ballistics Propulsion Dynamics Launch Dynamics Flight Dynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Ballistics categories.