Analysis of digital filters used in time-series small heat flux measurement

2022 ◽  
Vol 200 ◽  
pp. 117630
Author(s):  
Guoqiang Liu ◽  
Tong Xiong ◽  
Gang Yan ◽  
Jianlin Yu
2020 ◽  
Vol 1683 ◽  
pp. 022018
Author(s):  
S Z Sapozhnikov ◽  
V Y Mityakov ◽  
A Y Babich ◽  
E R Zainullina

2018 ◽  
Vol 89 (10) ◽  
pp. 10J122 ◽  
Author(s):  
J. Ren ◽  
D. Donovan ◽  
J. Watkins ◽  
H. Q. Wang ◽  
D. Rudakov ◽  
...  

2016 ◽  
Vol 17 (6) ◽  
pp. 925-931 ◽  
Author(s):  
Mohanapriya Venkataraman ◽  
Rajesh Mishra ◽  
V. Subramaniam ◽  
A. Gnanamani ◽  
T. M. Kotresh ◽  
...  

2015 ◽  
Vol 29 (1) ◽  
pp. 37-46 ◽  
Author(s):  
Benjamin Kraetzig ◽  
David R. Buttsworth ◽  
Fabian Zander ◽  
Stefan Löhle

2012 ◽  
Vol 152-154 ◽  
pp. 883-888
Author(s):  
Xiang Yu Zhang ◽  
Guo Qiang He ◽  
Pei Jin Liu ◽  
Jiang Li

Accurate information on heat transfer data of combustion products in the solid rocket motor chamber is a crucial prerequisite for the engine thermal protection. A measurement technique was well developed to acquire steady-state heat flux data of two-phase flow and was used successfully in the hostile environment. Experimental heat flux measurement has been obtained with an innovative designed instrument by simulating the flow field of complex charging configuration. The total heat flux of combustion products in the chamber was brought away by the coolant and calculated by its enthalpy rise in this device. The data could be used to analyze the heat transfer phenomena in SRMs and provide boundary condition for establishing insulation erosion model.


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