A calculation method for maximum steady-state loss of VSC-HVDC grounding resistor in Luxi back-back HVDC interconnector

2016 ◽  
Author(s):  
Weihuang Huang Weihuang Huang ◽  
Yuxin Lu Yuxin Lu ◽  
Xiaolin Li Xiaolin Li ◽  
Ying Huang Ying Huang ◽  
Shukai Xu Shukai Xu ◽  
...  
Keyword(s):  
Steady State ◽  
Calculation Method ◽  
Maximum Steady State

scholarly journals Gas turbine power calculation method of turboshaft based on simulation and performance model

2018 ◽  
Vol 189 ◽  
pp. 02003 ◽  
Author(s):  
Heng Wu ◽  
Shufan Zhao ◽  
Jijun Zhang ◽  
Bo Sun ◽  
Hanqiang Song
Keyword(s):  
Steady State ◽  
Combustion Chamber ◽  
Gas Turbine ◽  
Calculation Method ◽  
Performance Model ◽  
Power Calculation ◽  
Outlet Temperature ◽  
Acceptance Test ◽  
Test Drive ◽  
Turboshaft Engine

Gas turbine power of turboshaft engine cannot be measured, a total of five typical steady state point test data from the ground slow state to the maximum state were selected according to the factory acceptance test drive of a certain type of carrier-based helicopter turboshaft engine. Combustion chamber three-dimensional simulation model was established to carry on simulation analysis of different typical steady state combustion process. The simulated combustion chamber exit section parameters are input into the established gas turbine isentropic adiabatic aerodynamic calculation model to obtain the gas turbine power and outlet temperature. Select five typical steady state points of five sets of turboshaft engines on the same type to repeat the above calculation process, and compare the calculated value of gas turbine outlet temperature with the acceptance test values, it is found that the error values are all within 5%, and the effectiveness and accuracy of the gas turbine power calculation method are verified.

Prediction of sotalol-induced maximum steady-state QTc prolongation from single-dose administration in healthy volunteers

1992 ◽  
Vol 52 (4) ◽  
pp. 417-426 ◽  
Author(s):  
Franck Le Coz ◽  
Christian Funck-Brentano ◽  
Jean-Marie Poirier ◽  
Yves Kibleur ◽  
François Xavier Mazoit ◽  
...  
Keyword(s):  
Single Dose ◽  
Steady State ◽  
Healthy Volunteers ◽  
Qtc Prolongation ◽  
Dose Administration ◽  
Single Dose Administration ◽  
Maximum Steady State

Steady-State Thermal Analysis of a Thermometer Well

1963 ◽  
Vol 85 (3) ◽  
pp. 235-244 ◽  
Author(s):  
R. P. Benedict ◽  
J. W. Murdock
Keyword(s):  
Thermal Analysis ◽  
Steady State ◽  
Finite Difference ◽  
Balance Equation ◽  
Heat Balance ◽  
Calculation Method ◽  
Finite Difference Approximation ◽  
Difference Approximation ◽  
Differential Heat ◽  
Hand Calculation

A generalized thermometer well is analyzed as to temperature-measuring uncertainties. A reliable finite difference approximation to the differential heat balance equation is developed. For those cases where the fluid may be considered transparent to radiation (i.e., for εg ≈ 0), a simplified linearized approximation is given. Whenever conduction effects can be neglected (i.e., for (hc D/k)(L2/(D2 − d2)) > 20), a rapid hand-calculation method is indicated. Several examples of graphical approximations are given.

Study on Pilot Transfer Function Model Gain of Closed-Loop Pilot-Vehicle System

2013 ◽  
Vol 706-708 ◽  
pp. 1038-1041
Author(s):  
Lin Li ◽  
Jun Xu ◽  
Fu Lei Zheng
Keyword(s):  
Steady State ◽  
Transfer Function ◽  
Calculation Method ◽  
Closed Loop ◽  
Reference Value ◽  
Transfer Function Model ◽  
Function Model ◽  
Specific Calculation ◽  
Pilot Model ◽  
Vehicle System

Based on the analysis of pilot handling behavior characteristics, this paper establishes the pilot transfer function model. According to the characteristics of closed-loop pilot-vehicle system and the relationship between pilot and flight quality, the specific calculation method of pilot model steady state gain was given. Take the aircraft roll angle manipulation for example, and simulate the pilot's manipulation of aircraft of dynamic process. The results show that: the pilot model steady state gain calculation method is simple and feasible, and have a certain reference value for the analysis of closed-loop pilot-vehicle system.

A Model for Drying on Adiabatic Saturation Lines

1980 ◽  
Vol 102 (4) ◽  
pp. 347-351
Author(s):  
W. H. Hebrank
Keyword(s):  
Heat Transfer ◽  
Steady State ◽  
Computer Program ◽  
Calculation Method ◽  
Transfer Efficiency ◽  
Circulation Flow ◽  
Heat Transfer Efficiency ◽  
Process Cost ◽  
Flow Flux ◽  
Flow Quantity

A model is developed to simulate continuous steady state evaporation. The process is one that proceeds along adiabatic saturation curves. Aerodynamic effects of dryer air and circulation flow flux are combined with dryer temperature and humidity to compute evaporation rates. The calculation method requires several iteration loops and a computer program to do the work is described. Curves are presented of evaporation rates as affected by temperature, humidity, nozzle heat transfer efficiency and circulation flow quantity. Optimization of process cost and energy are discussed.

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