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The Aerodynamic Properties Of The 105mm He Shell Mi In Subsonic And Transonic Flight


The Aerodynamic Properties Of The 105mm He Shell Mi In Subsonic And Transonic Flight
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The Aerodynamic Properties Of The 105mm He Shell Mi In Subsonic And Transonic Flight


The Aerodynamic Properties Of The 105mm He Shell Mi In Subsonic And Transonic Flight
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Author : Eugene T. Roecker
language : en
Publisher:
Release Date : 1955

The Aerodynamic Properties Of The 105mm He Shell Mi In Subsonic And Transonic Flight written by Eugene T. Roecker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Ammunition categories.




The Aerodynamic Properties Of The 105mm He Shell M1 In Subsonic And Transonic Flight


The Aerodynamic Properties Of The 105mm He Shell M1 In Subsonic And Transonic Flight
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Author : EUGENE T. ROECKER
language : en
Publisher:
Release Date : 1955

The Aerodynamic Properties Of The 105mm He Shell M1 In Subsonic And Transonic Flight written by EUGENE T. ROECKER and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with categories.




Some Aerodynamic Properties Of A 105mm Model Of The 155mm T 358 Shell


Some Aerodynamic Properties Of A 105mm Model Of The 155mm T 358 Shell
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Author : W. E. Scott
language : en
Publisher:
Release Date : 1961

Some Aerodynamic Properties Of A 105mm Model Of The 155mm T 358 Shell written by W. E. Scott and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Ammunition categories.


The aerodynamic properties of a 105 mm model of the 155 mm T-358 shell are discussed. Subsonically, at small yaw, the model has a serious case of dynamic instability as indicated by a rapid divergence of the precessional component of yaw. It is shown that this instability is due to Magnus effects, and that these effects cannot be circumvented by firing at a different spin. However, because of past experience with similar shell, it is conjectured that this dynamic instability is a small yaw phenomenon and that a limit cycle is present. As a consequence of this, the dispersion will not be markedly affected.



Some Aerodynamic Properties Of Three 105mm Shell M1 T377 And T107


Some Aerodynamic Properties Of Three 105mm Shell M1 T377 And T107
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Author : Eugene D. Boyer
language : en
Publisher:
Release Date : 1958

Some Aerodynamic Properties Of Three 105mm Shell M1 T377 And T107 written by Eugene D. Boyer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Ammunition categories.




The Subsonic Aerodynamic Characteristics Of The 105mm He Shell M1 At Angles Of Attack From Zero To 180 Degrees


The Subsonic Aerodynamic Characteristics Of The 105mm He Shell M1 At Angles Of Attack From Zero To 180 Degrees
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Author : Robert L. McCoy
language : en
Publisher:
Release Date : 1974

The Subsonic Aerodynamic Characteristics Of The 105mm He Shell M1 At Angles Of Attack From Zero To 180 Degrees written by Robert L. McCoy and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Ammunition categories.




The Aerodynamic Properties Of The 155 Mm Shell M101 From Free Flight Range Tests Of Full Scale And 1 12 Scale Models


The Aerodynamic Properties Of The 155 Mm Shell M101 From Free Flight Range Tests Of Full Scale And 1 12 Scale Models
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Author : B. G. Karpov
language : en
Publisher:
Release Date : 1964

The Aerodynamic Properties Of The 155 Mm Shell M101 From Free Flight Range Tests Of Full Scale And 1 12 Scale Models written by B. G. Karpov and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.


The aerodynamic properties of the 155-mm HE Shell M101 as determined from Free Flight range firings of the full scale projectile and accurately scaled models 12.7 mm in diameter and semiscaled models of the same size are presented. It was found that at supersonic velocities, the aerodynamic characteristics are similar for the model and the full scale projectile. However, at lower transonic and subsonic velocities, the full scale data and the semiscaled model data differ. The accurately scaled model data may also be somewhat different from the full scale data, but the differences are considerably smaller than the differences shown by the semiscaled model data.



The Aerodynamic Properties Of A Spike Nosed Shell At Transonic Velocities


The Aerodynamic Properties Of A Spike Nosed Shell At Transonic Velocities
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Author : C. P. Sabin
language : en
Publisher:
Release Date : 1957

The Aerodynamic Properties Of A Spike Nosed Shell At Transonic Velocities written by C. P. Sabin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Ammunition categories.




Aerodynamic Properties Of A Family Of Shell Of Similar Shape 105mm Xm380e5 Xm380e6 T388 And 155mm


Aerodynamic Properties Of A Family Of Shell Of Similar Shape 105mm Xm380e5 Xm380e6 T388 And 155mm
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Author : Karolyn S. Krial
language : en
Publisher:
Release Date : 1970

Aerodynamic Properties Of A Family Of Shell Of Similar Shape 105mm Xm380e5 Xm380e6 T388 And 155mm written by Karolyn S. Krial and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.


The static and dynamic aerodynamic properties for a group of 5.6 caliber long shell with a 0.6 caliber eight degree boattail and a 2.9 caliber long secant ogive head are presented for a range of Mach number from 0.55 to 1.8. The four shells are the 105mm XM380E5, XM380E6, T388 and the 155mm T387. Stability properties of the 105mm versions are determined and their probable in-flight behavior discussed. (Author).



Aerodynamic Properties Of A Family Of Shell Of Similar Shape 105mm Xm380e5 Xm380e6 T388 And 155mm T387


Aerodynamic Properties Of A Family Of Shell Of Similar Shape 105mm Xm380e5 Xm380e6 T388 And 155mm T387
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Author :
language : en
Publisher:
Release Date : 1970

Aerodynamic Properties Of A Family Of Shell Of Similar Shape 105mm Xm380e5 Xm380e6 T388 And 155mm T387 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.


The static and dynamic aerodynamic properties for a group of 5.6 caliber long shell with a 0.6 caliber eight degree boattail and a 2.9 caliber long secant ogive head are presented for a range of Mach number from 0.55 to 1.8. The four shells are the 105mm XM380E5, XM380E6, T388 and the 155mm T387. Stability properties of the 105mm versions are determined and their probable in-flight behavior discussed. (Author).



Field Artillery Manual Cannon Gunnery


Field Artillery Manual Cannon Gunnery
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Author : Department of the Army
language : en
Publisher:
Release Date : 2017-08-19

Field Artillery Manual Cannon Gunnery written by Department of the Army and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2017-08-19 with categories.


Training Circular (TC) 3-09.81, "Field Artillery Manual Cannon Gunnery," sets forth the doctrine pertaining to the employment of artillery fires. It explains all aspects of the manual cannon gunnery problem and presents a practical application of the science of ballistics. It includes step-by-step instructions for manually solving the gunnery problem which can be applied within the framework of decisive action or unified land operations. It is applicable to any Army personnel at the battalion or battery responsible to delivered field artillery fires. The principal audience for ATP 3-09.42 is all members of the Profession of Arms. This includes field artillery Soldiers and combined arms chain of command field and company grade officers, middle-grade and senior noncommissioned officers (NCO), and battalion and squadron command groups and staffs. This manual also provides guidance for division and corps leaders and staffs in training for and employment of the BCT in decisive action. This publication may also be used by other Army organizations to assist in their planning for support of battalions. This manual builds on the collective knowledge and experience gained through recent operations, numerous exercises, and the deliberate process of informed reasoning. It is rooted in time-tested principles and fundamentals, while accommodating new technologies and diverse threats to national security.