Mechanical Analog Computer for Solving the Axial Equations of Motion during Bunching in Linear Electron Accelerators

1959 ◽  
Vol 30 (7) ◽  
pp. 543-547 ◽  
Author(s):  
P. T. Demos
Atomic Energy ◽  
1958 ◽  
Vol 4 (5) ◽  
pp. 583-589 ◽  
Author(s):  
G. A. Zeitlenok ◽  
V. V. Rumiantsev ◽  
V. L. Smirnov ◽  
L. P. Fumin ◽  
V. K. Khokhlov ◽  
...  

Nature ◽  
1948 ◽  
Vol 162 (4127) ◽  
pp. 890-890 ◽  
Author(s):  
R. B. R. SHERSBY HARVIE

2006 ◽  
Vol 1 ◽  
pp. 89-96
Author(s):  
Vadim L. Auslender ◽  
Vladimir V. Bezuglov ◽  
Aleksandr. A. Bryazgin ◽  
L. A. Voronin ◽  
V. A. Gorbunov ◽  
...  

2021 ◽  
pp. 136-141
Author(s):  
S.O. Bandurov ◽  
R.S. Lozhkin ◽  
G.О. Shyshkin

The article considers the ways to improve the protection system of linear electron accelerators ELV-1 and ELV-2 series on the basis of modern integrated and semiconductor component base. The proposed circuit solutions allowed turning off the facility power in case of gas electrical insulation breakdowns in the fast mode, that makes it impossible to work in an emergency. In order to improve the quality of control over the accelerator operation and additional informing an operator, capability of the proposed system to display information on the operator's computer monitor has been realized.


1975 ◽  
Vol 19 (04) ◽  
pp. 254-265
Author(s):  
Samuel H. Brown ◽  
Reidar Alvestad

This paper describes an analog computer maneuvering simulation of a destroyer study ship. The mathematical model used includes the ship propulsion machinery dynamics and the ship equations of motion. The model couples the ship propulsion dynamics equations with nonlinear maneuvering equations. The power plant representation consists of a simplified mathematical model of a General Electric LM2500 gas turbine engine and is primarily an engine mapping of engine torque versus engine speed using fuel flow. rate as a parameter. The simulation is used to accurately predict slow transients in ship speed during maneuvers resulting from slow increases in the fuel flow rate to the gas turbine. The advantage of the modified model presented in this paper over those not including propulsion dynamics is that it permits simulations of the effects of maneuvering on the propulsion plant.


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