Experimental modeling and uncertainty analysis of dispersed phase holdup at flooding in a pulsed disc-doughnut column, case study: Response surface methodology and Monte-Carlo simulation

2021 ◽  
Vol 141 ◽  
pp. 103969
Author(s):  
Benyamin Shakib ◽  
Ahad Ghaemi ◽  
Alireza Hemmati ◽  
Mehdi Asadollahzadeh
Keyword(s):  
Monte Carlo Simulation ◽  
Monte Carlo ◽  
Response Surface Methodology ◽  
Uncertainty Analysis ◽  
Response Surface ◽  
Experimental Modeling ◽  
Dispersed Phase

scholarly journals Modeling the uncertainty in response surface methodology through optimization and Monte Carlo simulation: An application in stamping process

2019 ◽  
Vol 173 ◽  
pp. 107776 ◽  
Author(s):  
Aneirson Francisco da Silva ◽  
Fernando Augusto Silva Marins ◽  
Erica Ximenes Dias ◽  
Jose Benedito da Silva Oliveira
Keyword(s):  
Monte Carlo Simulation ◽  
Monte Carlo ◽  
Response Surface Methodology ◽  
Response Surface ◽  
Stamping Process

Thermal Robustness and Mass Optimization of Heat Pipe Shape for Spacecraft Panel Using a Combination of Response Surface Methodology and Monte Carlo Simulation

2002 ◽  
Author(s):  
Takashi Kobayashi ◽  
Takehide Nomura ◽  
Masaki Kamifuji ◽  
Akira Yao ◽  
Tetsurou Ogushi
Keyword(s):  
Monte Carlo Simulation ◽  
Monte Carlo ◽  
Response Surface Methodology ◽  
Heat Pipe ◽  
Response Surface ◽  
Thermal Control ◽  
Optimization Method ◽  
Thermal Design ◽  
Design Parameters ◽  
Short Time

A commercial spacecraft should survive on orbit for more than 10 years under the severe circumstances without any maintenance. To realize this subject, not only performance but also other design factors such as reliability, mass, robustness, cost, etc. should be taken into consideration. From point of the thermal design, it is very important to obtain the robust thermal control subsystem with matrix heat pipe layout while minimizing the mass (weight). A new thermal optimization method without compromising the thermal robustness and the mass of thermal subsystem is highly anticipated. This paper proposes a robust thermal design approach for optimizing the heat pipe shape to minimize the mass of the spacecraft panel. We apply a combination of Design of Experiments (DOE), Response Surface Methodology (RSM) and Monte Carlo Simulation to determine the robust design parameters that minimize the mass of the heat pipe structure. Dimensions of the heat pipe design parameters were determined with rationally in a short time and practical robust optimization method was established.

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