Numerical analysis of heat transfer on the surface of a delta wing in a hypersonic air flow at large angles of attack

1985 ◽  
Vol 19 (5) ◽  
pp. 845-848
Author(s):  
N. E. Afonina ◽  
A. Yu. Vlasov ◽  
V. G. Gromov
1999 ◽  
Vol 123 (3) ◽  
pp. 315-318 ◽  
Author(s):  
Keiji Sasao ◽  
Mitsuru Honma ◽  
Atsuo Nishihara ◽  
Takayuki Atarashi

A numerical method for simulating impinging air flow and heat transfer in plate-fin type heat sinks has been developed. In this method, all the fins of an individual heat sink and the air between them are replaced with a single, uniform element having an appropriate flow resistance and thermal conductivity. With this element, fine calculation meshes adapted to the shape of the actual heat sink are not needed, so the size of the calculation mesh is much smaller than that of conventional methods.


Author(s):  
Nadia Dihmani ◽  
Ahmed Mezrhab ◽  
Larbi Elfarh ◽  
Hicham Bouali ◽  
Hassan Naji

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