Transient numerical simulation of annealing process in a conjugate combined radiation conduction heat transfer

2020 ◽  
Vol 27 (9) ◽  
pp. 2662-2672
Author(s):  
M. Foruzan Nia ◽  
S. A. Gandjalikhan Nassab
2014 ◽  
Vol 161 (10) ◽  
pp. 2692-2707 ◽  
Author(s):  
Andrea Brambilla ◽  
Christos E. Frouzakis ◽  
John Mantzaras ◽  
Ananias Tomboulides ◽  
Stefan Kerkemeier ◽  
...  

Author(s):  
Deepak Akhare ◽  
Hari Prasad Nandyala ◽  
Jayachandran T ◽  
Amit Kumar

Abstract In the present work, a complete 2D chemical and thermal non-equilibrium numerical model coupled with a relatively simple sheath model is developed for hydrogen arcjet thruster. Conduction heat transfer in the anode wall is also included in the model. The operating voltages predicted by the model are compared with those in the literature and are found to be in close agreement. Power distributions for the various operating conditions are obtained, anode radiation loss primarily determines the thruster efficiency. Higher thruster efficiency was found to be associated with longer arc length. At cathode ion diffusion contribution dominates except at low input current where thermo-field electron current is dominant.


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