scholarly journals Corrigendum to “Performance assessment of thermoelectric detector for heat flux measurement behind a reflected shock of low intensity” [Appl. Therm. Eng. 195 (2021) 117143]

2021 ◽  
Vol 199 ◽  
pp. 117609
Author(s):  
Mikhail A. Kotov ◽  
Andrey N. Shemyakin ◽  
Nikolay G. Solovyov ◽  
Mikhail Yu. Yakimov ◽  
Vladislav N. Glebov ◽  
...  
Author(s):  
Mikhail A. Kotov ◽  
Andrey N. Shemyakin ◽  
Nikolay G. Solovyov ◽  
Mikhail Yu. Yakimov ◽  
Vladislav N. Glebov ◽  
...  

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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